Publikationen

2022

R. Olmeda, F. Döhring, C. Stemmer: Study and Application of Wall-Roughness Models in LES Flows, International Journal of Heat and Fluid Flow, 94, 108948 (2022). DOI: 10.1016/j.ijheatfluidflow.2022.108948
J. M. F. Peter , M. J. Kloker: Direct numerical simulation of supersonic turbulent flow with film cooling by wall-parallel blowing, Physics of Fluids 34, 025125 (2022). DOI:10.1063/5.0080049

2021

Adams, N., Schröder, W., Radespiel, R., Haidn,O., Sattelmayer, T., Stemmer, C., Weigand, B.: Fundamental Technologies for the Development of Future Space Transportsystem Components under high Thermal and Mechanical Loads. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design book series (NNFM, volume 146), Springer Publishers, ISBN: 978-3-030-53847-7
Oskar J. Haidn, Nikolaus A. Adams, Rolf Radespiel, Thomas Sattelmayer, Wolfgang Schröder, Christian Stemmer, Bernhard Weigand: Collaborative Research for Future Space Transportation Systems. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design book series (NNFM, Volume 146), Springer Publishers, ISBN: 978-3-030-53847-7, pp 1-30.
Sholeh Karimghasemi, Siegfried Müller, Michael Westdickenberg, Flow solutions of transport equations
Communications in Partial Differential Equations, 46(1), 98--134, 2021, DOI: 10.1080/03605302.2020.1831018
Michael Herty, Siegfried Müller, Aleksey Sikstel, Coupling of Two Hyperbolic Systems by Solving Half-Riemann Problems,
in: Mathematical Modeling, Simulation and Optimization for Power Engineering and Management, S. Göttlich, M. Herty, A. Milde (Eds.), p. 285-302, Springer, 2021, DOI: 10.1007/978-3-030-62732-4
Valentina König, Michael Rom, Siegfried Müller, A Coupled Two-Domain Approach for Transpiration Cooling,
In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Future Space-Transport-System Components under High Thermal and Mechanical Loads, N. Adams, W. Schröder, R. Radespiel, O. Haidn, Th. Sattelmayer, C. Stemmer, B. Weigand, (Eds.), p. 33-49, Springer, 2021, DOI: 10.1007/978-3-030-53847-7
C. Gierden, J. Kochmann, J. Waimann, T. Kinner-Becker, J. Sölter, B. Svendsen, S. Reese: Efficient two-scale FE-FFT-based mechanical process simulation of elasto-viscoplastic polycrystals at finite strains. Computer Methods in Applied Mechanics and Engineering; Elsevier; 2021; Vol. 374, 113566, DOI: 10.1016/j.cma.2020.113566
S. Reese, T. Brepols, M. Fassin, L. Poggenpohl, S. Wulfinghoff: Using structural tensors for inelastic material modeling in the finite strain regime - A novel approach to anisotropic damage. Journal of the Mechanics and Physics of Solids; Elsevier; 2021; ISSN: 0022-5096; Vol. 146, 104174, DOI: 10.1016/j.jmps.2020.104174
O. Barfusz, T. van der Velden, T. Brepols, H. Holthusen, S. Reese: A reduced integration-based solid-shell finite element formulation for gradient-extended damage. Computer Methods in Applied Mechanics and Engineering; Elsevier; 2021; Vol. 382, 113884, DOI: 10.1016/j.cma.2021.113884
L. Poggenpohl, T. Brepols, H. Holthusen, S. Wulfinghoff, S. Reese: Towards brittle damage in carbon fiber reinforced plastics: A gradient extended approach. Composite Structures; Elsevier; 2021; ISSN: 0263-8223; Vol. 255, 112911, DOI: 10.1016/j.compstruct.2020.112911
O. Barfusz, T. Brepols, T. van der Velden, J. Frischkorn, S. Reese: A single Gauss point continuum finite element formulation for gradient-extended damage at large deformations. Computer Methods in Applied Mechanics and Engineering; Elsevier; 2021; Vol. 373, 113440, DOI: 10.1016/j.cma.2020.113440
O. Barfusz, F. Hoette, S. Reese, M. Haupt: Pseudo-transient 3D Conjugate Heat Transfer Simulation and Lifetime Prediction of a Rocket Combustion Chamber. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (Eds. N. Adams, W. Schröder, R. Radespiel, O. Haidn, T. Sattelmayer, C. Stemmer, B. Weigand); Springer; 2021; ISBN: 978-3-030-53847-7; ISSN: 1612-2909; Vol. 146, DOI: 10.1007/978-3-030-53847-7
O. Barfusz, T. van der Velden, T. Brepols, S. Reese: Towards forming simulations by means of reduced integration-based solid-shell elements considering gradient-extended damage. IOP Conference Series: Materials Science and Engineering (MSE); IOP Publishing; 2021; Vol. 1157, 012029, DOI: 10.1088/1757-899x/1157/1/012029
O. Barfusz, T. van der Velden, T. Brepols, S. Reese: Reduced integration-based solid and solid-shell finite elements for gradient-extended damage. Proceedings in Applied Mathematics and Mechanics; Wiley; 2021; submitted (June 14, 2021); 91th Annual Meeting of the International Association of Applied Mathematics and Mechanics, Kassel (Germany), March 15-19, 2021
V. Gerber, S. Baab, F.J. Förster, H. Mandler, B. Weigand, G. Lamanna: Fluid injection with supercritical reservoir conditions: Overview on morphology and mixing, The Journal of Supercritical Fluids, Vol. 169, 105097. DOI: https://doi.org/10.1016/j.supflu.2020.105097
C. Stemmer, R. Olmeda: Heat Exchange in Methane based Launchers. In: High Performance Computing in Science and Engineering – Garching/Munich 2020. Leibniz-Rechenzentrum (LRZ);Bayerische Akademie der Wissenschaften, 2021
R. Olmeda, C. Stemmer: LES of N2/H2 Transcritical Injection in a Rocket Combustion Chamber, In: New Results in Numerical and Experimental Fluid Mechanics XIII, Contributions to the 22nd STAB/DGLR Symposium, Eds: A.Dillmann, G.Heller, E.Krämer, C.Wagner, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol.151, 569-578, ISBN: 978-3-030-79560-3, 2022, Springer International Publishing

2020

Armbruster, W.; Hardi, J. S.; Miene, Y.; Suslov, D.; Oschwald, M.: Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines. Acta Astronautica 169
T. Brepols, S. Wulfinghoff, S. Reese: A gradient-extended two-surface damage-plasticity model for large deformations. International Journal of Plasticity; Elsevier; 2020; ISSN: 0749-6419; Vol. 129, 10263, DOI:10.1016/j.ijplas.2019.11.014
S. Loosen, M. Meinke, W. Schröder: Numerical Investigation of Jet-Wake Interaction for a Dual-Bell Nozzle. Flow Turbul. Combust. 104.2 (2020), pp. 553–578
Dirk Schneider, Ralf Stark, Chloé Génin, Michael Oschwald, Konstantin Kostyrkin: Active Control of Dual-Bell Nozzle Operation Mode Transition by Film Cooling and Mixture Ratio Variation. Journal of Propulsion and Power Vol. 36, No. 1, pp. 47-58, 2020
V. Gerber, S. Baab, B. Weigand, G. Lamanna: Enhanced Rayleigh scattering in supercritical fluid injection across the Widom line, Atomization and Sprays, Vol. 30, No. 12, pp. 881–893, DOI: 10.1615/AtomizSpr.2020035322.
Raffaele Olmeda, Christian Stemmer: LES of N2/H2 Transcritical Injection in a Rocket Combustion Chamber. In: New Results in Numerical and Experimental Fluid Mechanics XIII Book Subtitle: Contributions to the 22nd STAB/DGLR Symposium. Springer International Publishing, 2021

2019

König, V., Müller, S., Rom, M.: Numerical investigation of transpiration cooling in supersonic nozzles, 8th European Conference for Aeronautics and Space Sciences
Michael Herty, Siegfried Mueller, Aleksey Sikstel: Coupling of compressible Euler equations. Vietnam Journal of Mathematics
Ludescher, S.; Olivier, H.: Use of a detonation tube for investigation of the mixing effects of hot gas and coolant in a film cooled nozzle. 32nd Int. Symposium on Shock Waves, Singapore, July 2019, 2067-2078
David J. Munk, Markus Selzer, Grant P. Steven, and Gareth A. Vio: Topology Optimization Applied to Transpiration Cooling. AIAA Journal 2019 57(1), 297-312
Saile, D.; Kühl, V.; Gülhan, A.: On the subsonic near-wake of a space launcher configuration without jet. Experiments in Fluids, 60(4)
Saile, D.; Kühl, V.; Gülhan, A.: On the subsonic near-wake of a space launcher configuration with exhaust jet. Experiments in Fluids, 60(165)
Saile, D.; Kühl, V.; Gülhan, A.: On Subsonic Near-Wake Flows of a Space Launcher Configuration with Various Base Geometries. 13th International Symposium on Particle Image Velocimetry - ISPIV 2019, 22-24 July, Munich, Germany
Saile, D.: Experimental Analysis on Near-Wake Flows of Space Transportation Systems. Ph.D. Thesis, RWTH Aachen
Kirchheck, D.; Saile, D.; Gülhan, A.: Spectral Analysis of Rocket Wake Flow-Jet Interaction by Means of High-speed Schlieren Imaging. Title of Coference:8th European Conference for Aeronautics and Space Sciences (EUCASS), 1-4 July, Madrid, Spain
Istvan Bolgar, Sven Scharnowski, Christian J. Kähler: Passive Flow Control for Reduced Load Dynamics Aft of a Backward-Facing Step. AIAA Journal.
Istvan Bolgar, Sven Scharnowski, Christian J. Kähler: Experimental analysis of the interaction between a Dual-Bell nozzle with an external flow field aft of a backward-facing step. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design: Tagungsband des 21. DGLR-Fachsymposium der STAB
Christoph Traxinger, Julian Zips, Michael Pfitzner: Single-Phase Instability in Non-Premixed Flames Under Liquid Rocket Engine Relevant Conditions. Journal of Propuslion and Power.
Julian Zips, Christoph Traxinger, Paola Breda, Michael Pfitzner: Assessment of Presumed/Transported Probability Density Function Methods for Rocket Combustion Simulations. Journal of Propulsion and Power.
Chemnitz, A., Kings, N., Sattelmayer, T.: Modification of Eigenmodes in a Cold-Flow Rocket Combustion Chamber by Acoustic Resonators. Journal of Propulsion and Power.
F. Föll, T. Hitz, C. Müller, C.-D. Munz, M. Dumbser: On the use of tabulated equations of state for multi-phase simulations in the homogeneous equilibrium limit. Shock waves - Springer.
Gröning, S.; Hardi, J.S.; Suslov, D.; Oschwald, M.: Measuring the Phase Between Fluctuating Pressure and Flame Radiation Intensity in a Cylindrical Combustion Chamber. Progress in Propulsion Physics 11
Armbruster, W.; Hardi, J.; Miene, Y.; Suslov, D.; Oschwald, M.: LOX Injector Geometry Changes to Reduce the Risk of Injection-Coupled Combustion Instabilities in a Cryogenic Rocket Thrust Chamber. 32nd ISTS (International Symposium on Space Technology and Science), Fukui Japan.
Armbruster, W.; Hardi, J.S.; Suslov, D.; Oschwald, M.: Injector-Driven Flame Dynamics in a High-Pressure Multi-Element Oxygen–Hydrogen Rocket Thrust Chamber. Journal of Propulsion and Power 35.
O. Barfusz, T. Brepols, J. Frischkorn, S. Reese: Towards the incorporation of damage into solid-shells based on reduced integration. Title of Journal: Proceedings in Applied Mathematics and Mechanics. 90th Annual Meeting of the International Association of Applied Mathematics and Mechanics.
M. Fassin, R. Eggersmann, S. Wulfinghoff, S. Reese: Gradient-extended anisotropic brittle damage modeling using a second order damage tensor – Theory, implementation and numerical examples. International Journal of Solids and Structures.
M. Fassin, R. Eggersmann, S. Wulfinghoff, S. Reese: Efficient algorithmic incorporation of tension compression asymmetry into an anisotropic damage model. Computer Methods in Applied Mechanics and Engineering.
Hötte, F.; Lungu, P.; von Sethe, C.; Fiedler, T.; Haupt, M.C.; Haidn, O.: Experimental Investigations of Thermo-Mechanical Fluid-Structure Interaction in Rocket Combustion Chambers. Journal of Propulsion and Power.
S. Loosen, M. Meinke, W. Schröder. Numerical investigation of jet-wake interaction for a generic space launcher with a dual-bell nozzle. In: Proceedings of the 8th European Conference for Aeronautics and Aerospace Sciences, Madrid, Spain. 2019
R. Olmeda, C. Stemmer: Wall Heat Flux Analysis of a Film-Cooled Single-Element Combustion Chamber with Large-Eddy Simulations. 32nd International Symposium on Shock Waves , 2019, ISSW32 Singapore

2018

König, V.; Mueller, S.; Rom, M.: Influence of non-uniform injection into a transpiration-cooled turbulent channel flow: A numerical study. AIAA Science and Technology Forum and Exposition.
Herty, M.; Mueller, S.; Gerhard, N.; Xiang, G.; Wang, B.: Fluid-structure coupling of linear elastic model with compressible flow models. International Journal for Numerical Methods in Fluids.
M. Herty, S. Mueller, A. Sikstel: Fluid-structure coupling of a linear elastic model with a compressible flow model with multilevel timestepping. 6th ECCOMAS Conference on Computational Mechanics, 7th European Conference on Computational Fluid Dynamics
Valentina König, Michael Rom, S.M., Markus Selzer, Sven Schweikert, Jens von Wolfersdorf: Numerical and experimental investigation of transpiration cooling with C/C characteristic outflow distributions. Journal of Thermophysics and Heat Transfer.
Giulia Deolmi, Siegfried Mueller: A two-step model order reduction method to simulate a compressible flow over an extended rough surface. Mathematics and Computers in Simulation.
Ludescher, S.; Olivier, H.: Experimental Investigations of Film Cooling Behavior under Rocket-Engine-Like Flow Conditions. 2018 AIAA Aerospace Sciences Meeting
Ludescher, S.; Olivier, H.: Experimental Investigations of Film Cooling in a Conical Nozzle Under Rocket-Engine-Like Flow Conditions. AIAA Journal.
Wenzel, C.; Selent, B.; Kloker, M.; Rist, U.: DNS of compressible turbulent boundary layers and assessment of data/scaling-law quality. J. Fluid Mech.
David J. Munk, Markus Selzer, Hannah Böhrk, Sven Schweikert and Gareth A. Vio: "Numerical Modeling of Transpiration-Cooled Turbulent Channel Flow with Comparisons to Experimental Data". Journal of Thermophysics and Heat Transfer 2018 32:3, 713-735.
Barklage, A., Radespiel, R., Genin, C.: Afterbody jet interaction of a dual-bell nozzle in supersonic flow. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4468.
A. Barklage, R. Radespiel: Influence of the boundary layer state on the transition of a dual-bell nozzle. Deutscher Luft- und Raumfahrtkongress.
Istvan Bolgar, Sven Scharnowski, Christian J. Kähler: The Effect of the Mach Number on a Turbulent Backward-Facing Step Flow. Flow, Turbulence and Combustion.
Istvan Bolgar, Sven Scharnowski, Christian J. Kähler: Experimental analysis of the interaction between a Dual-Bell nozzle with an external flow field aft of a backward-facing step. 21. DGLR-Fachsymposium der STAB.
Traxinger, C., Zips, J., Pfitzner, M.: Thermodynamic analysis and large-eddy simulations of LOx-CH4 and LOx-H2 flames at high pressure. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4765.
Christoph Traxinger, Julian Zips, Michael Pfitzner: Numerische Untersuchung von Phasengleichgewichten bei der Injektion und Verbrennung in Flüssigkeitsraketentriebwerken. Thermodynamik Kolloquium, Kassel.
Christoph Traxinger, Matthias Banholzer, Michael Pfitzner: Real-Gas Effects and Phase Separation in Underexpanded Jets at Engine-Relevant Conditions. AIAA SciTech Forum, Kissimmee, Florida, AIAA paper 2018-1815.
Chemnitz, A., Kings, N., Sattelmayer, T.: Modification of Eigenmodes in a Rocket Combustion Chamber by Acoustic Resonators under Non-Reacting Conditions. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4950.
A. Chemnitz, T. Sattelmayer, C. Roth, O. Haidn, Y. Daimon, R. Keller, P. Gerlinger, J. Zips, M. Pfitzner: Numerical Investigation of Reacting Flow in a Methane Rocket Combustor: Turbulence Modeling. Journal of Propulsion and Power.
F. Föll, S. Pandey, X. Chu, C.-D. Munz, E. Laurien, B. Weigand:High-fidelity direct numerical simulation of supercritical channel flow using discontinuous Galerkin spectral element method. High Performance Computing in Science and Engineering - Springer Verlag.
Förster, F.J., Baab, S., Steinhausen, C., Lamanna, G., Ewart, P., Weigand, B.: Mixing characterization of highly underexpanded fluid jets with real gas expansion. Exp. Fluids, Vol. 59(44).
Chang, W., Chu, X., Fareed, A. F. B. S., Pandey, S., Luo, J., Weigand, B., & Laurien, E.: Heat transfer prediction of supercritical water with artificial neural networks. Applied Thermal Engineering.
Pandey, S., Chu, X., Laurien, E., & Weigand, B.: Buoyancy induced turbulence modulation in pipe flow at supercritical pressure under cooling conditions. Physics of Fluids.
Zips, J., Müller, H., Pfitzner, M.: Efficient thermo-chemistry tabulation for non-premixed combustion at high-pressure conditions. Flow, Turbulence and Combustion.
Beinke, S., Hardi, J., Oschwald, M., Banuti, D., Karl, S., Dally, B.: Experimental and numerical study of oxygen-hydrogen rocket flame response to transverse acoustic excitation. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4947.
Tonti, F., Hardi, J., Karl, S., Oschwald, M.: Unsteady Modelling of LOx/GH2 Flame Response to Longitudinal Chamber Mode Forcing. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4949.
Kostyrkin, K., Schneider, D., Stark, R., Genin, C., Oschwald, M.: Operation Mode Transition of Film-Cooled Dual-Bell Nozzles. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4467.
Armbruster, W.; Hardi J. S.; Suslov, D.; Oschwald, M.: Experimental investigation of self-excited combustion instabilities with injection coupling in a cryogenic rocket combustor. Acta Astronautica 151.
O. Barfusz, R. Smeenk, S. Reese: Solid-shells based on reduced integration - geometrically non-linear analysis of layered structures. Title of Journal: Proceedings of the 6th European Conference of Computational Mechanics.6th European Conference of Computational Mechanics.
O. Barfusz, R. Smeenk, S. Reese: Solid-shell formulations based on reduced integration - investigations of anisotropic material behaviour at large deformations. Proceedings in Applied Mathematics and Mechanics. 89th Annual Meeting of the International Association of Applied Mathematics and Mechanics
Doehring, A., Adams, N: Numerical Investigation of Transcritical Turbulent Channel Flow. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4768.
Thomas Kaller, Vito Pasquariello, Stefan Hickel, Nikolaus A. Adams: Turbulent flow through a high aspect ratio cooling duct with asymmetric wall heating. Journal of Fluid Mechanics.
Thomas Kaller, Stefan Hickel, Nikolaus A. Adams: LES of an Asymmetrically Heated High Aspect Ratio Duct at High Reynolds Number at Different Wall Temperatures. 2018 Joint Thermophysics and Heat Transfer Conference, AIAA AVIATION Forum, AIAA 2018-4287.
Scholz, P.; Rochlitz, H.: The turbulent velocity and temperature field in a heated duct. 5th International Conference on Experimental Fluid Mechanics, ICEFM 2018 2-4 July 2018, München.
Rochlitz, H.; Scholz, P.: Application of laser-induced fluorescence technique in a duct flow with one heated wall. Experiments in Fluids, Vol 59 (3), p.54.
Hötte, F., Lungu, P., Haupt, M., Haidn, O.: Experimental and numerical investigations of thermo-mechanical fluid-structure interaction in cooled rocket combustion chambers. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4767.
Daimon, Y., Negishi, H., Silvestri, S., Haidn, O.: Conjugated Combustion and Heat Transfer Simulation for a 7 element GOX/GCH4 Rocket Combustor. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4553.
Perakis, N., Haidn, O., Eiringhaus, D., Rahn, D., Zhang, S., Daimon, Y.:Qualitative and Quantitative Comparison of RANS Simulation Results for a 7-Element GOX/GCH4 Rocket Combustor. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4556.
Perakis, N., Rahn, D., Eiringhaus, D., Haidn, O.: Heat Transfer and Combustion Simulation of a 7-Element GOX/GCH4 Rocket Combustor. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4554.
Silvestri, S., Lungu, P., Kirchberger, C., Haidn, O.: Axial and Azimuthal Heat Load Distribution in 7-Injector GOX/GCH4 Combustion Chamber. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4552.
Sternin, A., Perakis, N., Haidn, O., Tajmar, M.: CFD-Analysis of the film cooling influence on the main flow and wall heat flux in a GCH4/GOX rocket combustion chamber with a square-shaped cross section. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4766.
Zhang, S., Wei, J., Qin, J., Ye, M., Haidn, O.: Modelling of a 7-Elements GOX/GCH4 Combustion Chamber Using RANS with EDC Combustion Model. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4555.
Winter, F., Perakis, N., Haidn, O.: Emission imaging and CFD simulation of a coaxial single-element GOX/GCH4 rocket combustor. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4764.
Barklage, A., Radespiel, R., Génin, C.:Afterbody jet interaction of a dual-bell nozzle in supersonic flow. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4468.
Takahashi, H., Tomita, T., Génin C. and Schneider, D.: LOX/CH4 Hot-Flow Testing of Dual-Bell Nozzles with Rapid-Expansion Extension. Journal of Propulsion and Power.
Stark, R., Génin, C., Mader, C., Maier, D., Schneider, D. and Wohlhüter, M.: Design of a Film Cooled Dual-Bell Nozzle. Acta Astronautica.
Schneider, D., Génin C., Stark R., Oschwald, M., Karl S., Hannemann, V.: Numerical Model for Nozzle Flow Application Under Liquid Oxygen/Methane Hot-Flow Conditions. Journal of Propulsion and Power 34(1), pp. 221-233.
Schneider, D., Stark, R.H., Génin, C., Oschwald, M., Kostyrkin, K.: Operation Mode Transition of Film-Cooled Dual-Bell Nozzles.2018 AIAA Propulsion and Energy Forum, AIAA-2018-4467.
Armbruster, W., Hardi, J., Suslov, D., Oschwald, M.: High-Speed Flame Radiation Imaging of Thermoacoustic Coupling in a High Pressure Research Thrust Chamber. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4951.
Eiringhaus, D., Riedmann, H., Knab, O., Haidn, O.: Full-Scale Virtual Thrust Chamber Demonstrators as Numerical Testbeds within SFB-TRR 40. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4469.
Perakis, N., Haidn, O., Eiringhaus, D., Rahn, D., Zhang, S., Daimon, Y.: Qualitative and Quantitative Comparison of RANS Simulation Results for a 7-Element GOX/GCH4 Rocket Combustor. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4556.
Perakis, N., Rahn, D., Eiringhaus, D., Haidn, O.: Heat Transfer and Combustion Simulation of a 7-Element GOX/GCH4 Rocket Combustor. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4554.
Eiringhaus, D., Riedmann, H., Knab, O. and Haidn, O.J.: 3D RANS Simulations of Full-Scale Liquid Rocket Thrust Chambers. Space Propulsion Conference 2018.
Haidn,O., Adams, N., Stemmer, C., Sattelmayer, T., Radespiel, R., Schröder, W., Weigand, B.: Fundamental Technologies for the Development of Future Space Transportsystem Components under high Thermal and Mechanical Loads. 2018 AIAA Propulsion and Energy Forum, AIAA-2018-4466.
S. Loosen, V. Statnikov, M. Meinke, W. Schröder. Numerical Investigation of the Turbulent Wake of Generic Space Launchers. In: High Performance Computing in Science and Engineering ’ 17. Ed. by W. E. Nagel, D. H. Kröner & M. M. Resch. 2018, pp. 289–304
S. Loosen, V. Statnikov, M. Meinke, W. Schröder. Modal analysis of passive flow control for the turbulent wake of a generic planar space launcher. CEAS Space J. 10.2 (2018), pp. 189–202

2017

König, V., Dahmen, W., Müller, S., Rom, M.: Numerical investigation of transpiration cooling with uniformly and non-uniformly simulated injection. 7th European Conference for Aeronautics and Space Sciences 3-6 July, 2017 - Milan (ITALY).
Haase, S., Olivier, H.: Influence of condensation on heat flux and pressure measurements in a detonation-based short-duration facility. Experiments in Fluids.
Caeiro, F., Sovardi, C., Förner, K., Polifke, W.: Shape Optimisation of a Helmholtz Resonator using an Adjoint Method. International Journal of Spray and Combustion Dynamics.
Förner, K., Polifke, W.: Nonlinear Aeroacoustic Identification of Helmholtz Resonators Based on a Local-Linear Neuro-Fuzzy Network Model. Journal of Sound and Vibration.
Peter, J.M.F.; Kloker, M.J.: Preliminary work for DNS of rocket-nozzle film cooling. Deutscher Luft- und Raumfahrtkongress, Paper DLRK-2017-450178.
Kirchheck, D.; Gülhan, A.: Interaktionsteststand für realistische Raketentreibstrahlen mit umströmender Atmosphäre. Deutscher Luft- und Raumfahrtkongress, 5-7 Sept, Munich, Germany.
Statnikov, V., Meinke, M., Schröder, W.: Reduced-order analysis of buffet flow of space launchers. J. Fluid Mech., 815, 1-25(2017).
S. Stephan, R. Radespiel: Propulsive jet simulation with air and helium in launcher wake flows. CEAS Space Journal, 9, Issue 2, pp.195-209.
A.Barklage, S. Loosen, I. Bolgar, R. Radespiel, W. Schröder, C. Kähler: Experimental and numerical investigation of passive flow control devices on a generic space launcher. Deutscher Luft- und Raumfahrtkongress.
Istvan Bolgar, Sven Scharnowski, Christian J. Kähler: Correlations between turbulent wall pressure and velocity field fluctuations in backward-facing step flows. Deutscher Luft- und Raumfahrtkongress 2017.
Kings, N., Chemnitz, A., Schulze, M., Sattelmayer, T.: On the Effect of Acoustic Absorbers Coupled to Rocket Combustors. 7th European Conference for Aeronautics and Space Sciences.
Chemnitz, A., Kings, N., Schulze, M., Sattelmayer, T.: Numerical Investigation of Eigenmode Damping Rates in a Single Element Rocket Combustion Chamber. 31st International Symposium on Space Technology and Science.
Schulze, M., Sattelmayer, T.: Linear Stability Assessment of a Cryogenic Rocket Engine. International Journal of Spray and Combustion Dynamics.
Hardi, J. S., Traudt, T., Bombardieri, C., Börner, M., Beinke, S. K., Armbruster, W., Blanco, P. N., Tonti, F., Suslov, D., Dally, B., Oschwald, M.: Combustion dynamics in cryogenic rocket engines: research programme at DLR Lampoldshausen. International Astronautical Congress (IAC).
Armbruster, W., Hardi, J. S., Suslov, D., Oschwald, M.: Experimental Investigation of Self-Excited Combustion Instabilities with Injection Coupling in a Cryogenic Rocket Combustor. International Astronautical Congress (IAC).
Fiala, T.; Sattelmayer, T.; Gröning, S.; Hardi, J.; Stützer, R.; Webster, S., Oschwald, M.: Comparison Between Excited Hydroxyl Radical and Blue Radiation from Hydrogen Rocket Combustion. Journal of Propulsion and Power.
Armbruster, W., Hardi, J., Oschwald, M.: Experimentelle Untersuchung selbsterregter Verbrennungsinstabilitäten in einer LOX/H2 Raketenbrennkammer. Deutscher Luft- und Raumfahrtkongress (DLRK) 2017.
Fiedler, T., Bäker, M., Rösler, J.: Large Heat Flux Exposure of Metallic Coatings for Rocket Engine Application. Surface & Coatings Technology. International Conference on Metallurgical Coatings and Thin Films.
Fiedler, T., Groß, R., Rösler, J., Bäker, M.: Damage mechanisms of metallic HVOF-coatings for high heat flux application. Surface & Coatings Technology.
Wulfinghoff,S., Fassin, M., Reese, S.: A damage growth criterion for anisotropic damage models motivated from micromechanics. International Journal of Solids and Structures.
Barfusz, O., Schwarze, M., Reese, S.: Numerical investigations of CMC nozzle structures: constitutive modelling and finite element technology. Proceedings in Applied Mathematics and Mechanics. 89th Annual Meeting of the International Association of Applied Mathematics and Mechanics.
S. Reese, O. Barfusz, M. Schwarze, J.-W. Simon: Solid-shell formulations based on reduced integration - investigations of anisotropic material behaviour, large deformation problems and stability. Proceedings of the 11th International Conference on Shell Structures (SSTA 2017). Shell Structures, Theory and Applications.
Kaller, T.; Pasquariello, V.; Hickel, S.; Adams, N. A.: Numerical Investigation of the flow field in a high-aspect-ratio cooling duct. Deutscher Luft- und Raumfahrtkongress 2017.
Kaller, T.; Pasquariello, V.; Hickel, S.; Adams, N. A.: Large-eddy simulation of the high-Reynolds-number flow through a high-aspect-ratio cooling duct. 10th International Symposium on Turbulence and Shear Flow Phenomena (TSFP10).
Simona Silvestri, Christoph Kirchberger, Gregor Schlieben, Maria Palma Celano, Oskar Haidn: Experimental and Numerical Investigation of a Multi-Injector GOX-GCH4 Combustion Chamber. 31st Int. Symposium on Space Technology and Science.
Fernanda Winter, Simona Silvestri, Maria Palma Celano Gregor Schlieben, Oskar Haidn: High-speed and Emission Imaging of a Coaxial Single Element GOX/GCH4 Rocket Combustion Chamber.
Simona Silvestri, Fernanda Winter, Maria Palma Celano, Gregor Schlieben, Oliver Knab, Oskar Haidn: Investigation on Recess Variation of a Shear Coax Injector in a GOX-GCH4 Rectangular Combustion Chamber with Optical Access.
Stark, R., Génin, C., Mader, C., Maier, D., Schneider, D., Wohlhüter M.: Design of a Film Cooled Dual-Bell Nozzle. 7th European Conference for Aeronautics and Space Science Scopus.
Eiringhaus, D., Rahn, D., Riedmann, H., Knab, O. and Haidn, O.: Numerical Investigation of a 7-Element GOX/GCH4 Subscale Combustion Chamber. 7th European Conference for Aeronautics and Aerospace Sciences (EUCASS).
S. Loosen, V. Statnikov, M. Meinke, W. Schröder. Numerical investigation of the turbulent wake of a generic space launcher at transonic speed. In: Proceedings of the 7th European Conference for Aeronautics and Aerospace Sciences, Milano, Italy. 2017
Traxinger, C.; Müller, H.; Pfitzner, M.; Baab, S.; Lamanna, G.; Weigand, B.; Matheis, J.; Stemmer, C.; Adams, N.A.; Hickel, S.: Experimental and Numerical Investigation of Phase Separation due to Multi-Component Mixing at High-Pressure Conditions. ILASS2017 - 28th European Conference on Liquid Atomization and Spray Systems, 2017

2016

D. Broersen, W. Dahmen, R.: Stevenson On the Stability of DPG Formulations of Transport Equations. Mathematics of Computation, DOI:10.1090/mcom/3242.
G. Deolmi, W. Dahmen, S. Müller: Effective boundary conditions: a general strategy and application to compressible flows over rough boundaries. Communications in Computational Physics, 21(2), 358-400, 2017.
Tournadre, J., Förner, K., Polifke, W., Martinez-Lera, P., Desmet, W.: Determination of Acoustic Impedance for Helmholtz Resonators Through Incompressible Unsteady Flow Simulations. 22nd AIAA/CEAS Aeroacoustics Conference.
Förner, K., Tournadre, J., Martinez-Lera, P., Polifke, W.: Scattering to Higher Harmonics for Quarter Wave and Helmholtz Resonators. 22nd AIAA/CEAS Aeroacoustics Conference .
Caeiro, F., Sovardi, C., Förner, K., Polifke, W.: Shape Optimisation of a Helmholtz Resonator using the Adjoint Method. Int. Symposium on Thermoacoustic Instabilities in Gas Turbines and Rocket.
J. Tournadre, K. Förner, W. Polifke, P. Martínez-Lera, W. Desmet: Determination of Acoustic Impedance for Helmholtz Resonators Through Incompressible Unsteady Flow Simulations. AIAA Journal.
K. Förner, J. Tournadre, P. Martínez-Lera, W. Polifke: Scattering to Higher Harmonics for Quarter Wave and Helmholtz Resonators. AIAA Journal.
J. Tournadre, K. Förner, W. Polifke, P. Martínez-Lera, W. Desmet: Influence of Vortex Disruption on the Nonlinear Acoustic Response of Orifices. Journal of Sound and Vibration.
S. Jaensch, M. Merk, E. Gopalakrishnan, S. Bomberg, T. Emmert, R. I. Sujith, W. Polifke: Hybrid CFD/ Low-Order Modeling of Nonlinear. Thermoacoustic Oscillations. Proceedings of the Combustion Institute 36.
Keller, M.A., Kloker, M.J.: Direct Numerical Simulation of Foreign-Gas Film Cooling in Supersonic Boundary-Layer Flow. AIAA-Journal.
Keller, M.A., Kloker, M.: Direct Numerical Simulation of Foreign-Gas Film Cooling in Supersonic Boundary-Layer Flow. AIAA-Journal
Groskopf, G., Kloker, M.: Instability and transition mechanisms induced by skewed roughness elements in a high-speed laminar boundary layer. J. Fluid Mechanics
Stefan Löhle, Sven Schweikert, Jens von Wolfersdorf: A Method for Surface Heat Flux Determination of a Transpiration Cooled Wall from Pressure Data. Journal of Thermophysics and Heat Transfer.
Sven Schweikert, Stefan Löhle , Markus Selzer, Hannah Böhrk, Jens von Wolfersdorf: Surface Heat Flux Determination of Transpiration Cooled C/C by the Application of Non-integer System Identification. 8th European Workshop on Thermal Protection Systems and Hot Structures, ESA/ESTEC, Noordwijk, The Netherlands
Dittert, C.; Selzer, M.; Böhrk, H.: Flow Field and Pressure Decay Analysis of Porous Cones. AIAA Journal.
Kevin Basore, Markus Selzer, Vincent Wheatley, Russell R. Boyce, David J. Mee, Bianca R. Capra, Markus Kuhn, Stefen Brieschenk: Performance Comparison of Distributed Injection Methods for Hypersonic Film-Cooling. 20th Australasian Fluid Mechanics Conference, 5.-8. Dez. 2016, Perth, Australien.
Statnikov, V., Roidl, B., Meinke, M., Schröder, W.: Analysis of spatio-temporal wake modes of space launchers at transonic flow. AIAA SciTech, San Diego, United States, 4-8 Jan. 2016.
Statnikov, V; Bolgar, I; Scharnowski, S; Meinke, M; Kähler, C.J; Schröder, W.: Analysis of characteristic wake flow modes on a generic transonic backward-facing step configuration. Euro J Mech Fluids.
Statnikov, V., Meinke, M., Schröder, W.: Spatio-temporal analysis of transonic wake flows of space launchers via zonal RANS-LES and DMD. ETMM11.
Statnikov, V., Roidl, B., Meinke, M., Schröder, W.: Analysis of spatio-temporal wake modes of space launchers at transonic flow. AIAA SciTech.
Statnikov, V., Stephan, S., Pausch, K., Meinke, M., Radespiel, R., Schröder, W.: Experimental and numerical investigations of the turbulent wake flow of a generic space launcher at M = 3 and M = 6. CEAS Space Journal.
Schreyer, A.-M.; Stephan, S.; Radespiel, R.:Flow structure and unsteadiness in the supersonic wake of a generic space launcher. AIAA Science and Technology Forum and Exposition.
A.‐M. Schreyer, S. Stephan, R. Radespiel: Characterization of the supersonic wake of a generic space launcher. CEAS Space Journal.
Istvan Bolgar, Sven Scharnowski, Christian J. Kähler: Control of the Reattachment Length of a Transonic 2D Backward-Facing Step Flow. Springer Proceedings in Physics: Proceedings of the 5th International Conference on Jets, Wakes and Separated Flows (ICJWSF2015).
Sven Scharnowski, Istvan Bolgar, Christian J. Kähler: Untersuchungen der Heckströmung eines generischen Raketenmodells im Unter-, Trans-, und Überschall. Experimentelle Strömungsmechanik 24. Fachtagung.
Sven Scharnowski, Istvan Bolgar, Christian J. Kähler:Characterization of turbulent structures in a transonic backward-facing step flow. Flow, Turbulence and Combustion.
Müller H., Zips J., Pfitzner M., Maestro D.,Cuenot B., Selle L., Ranjan R., Tudisco P., Menon S.: Numerical Investigation of Flow and Combustion in a Single-Element GCH4/GOX Rocket Combustor: A comparative LES study. 52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Roth C., Haidn O., Chemnitz A., Sattelmayer T., Daimon Y., Frank G., Müller H., Zips J., Pfitzner M., Keller R., Gerlinger P., Maestro D., Cuenot B., Riedmann H., Selle L.: Numerical Investigation of Flow and Combustion in a Single-Element GCH4/GOX Rocket Combustor. 52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Traxinger C., Müller H., Pfitzner M.: Numerische Untersuchung des transkritischen Phasenzerfalls bei trans- und überkritischer Einspritzung. Thermodynamik-Kolloquium.
Müller H., Pfitzner M.: A flamelet model for transcritical LOx/GCH4 flames. NICFD conference.
Müller H., Pfitzner M.: Large-eddy simulations of a piloted jet flame with inhomogeneous inlets using a flamelet/progress variable approach.13th TNF workshop.
Müller H., Pfitzner M.: Large-eddy simulation of methane/oxygen combustion at supercritical pressure. 36th Combustion Symposium.
Zahn, M., Schulze, M., Hirsch, C., Sattelmayer, T.: Impact of Quarter Wave Tube Arrangement on Damping of Azimuthal Modes. ASME Turbo EXPO.
Schulze, M., Sattelmayer, T.: Linear Stability Assessment of a Cryogenic Rocket Engine. International Symposium on Thermoacoustic Instabilities in Gas Turbines and Rocket Engines.
Schulze, M., Schmid, M., Sattelmayer, T.: Influence of Atomization Quality Modulation on Flame Dynamics in a Hypergolic Rocket Engine. International Journal of Spray and Combustion Dynamics.
Kaess, R., Köglmeier, S., Sattelmayer, T., Schulze, M., Oschwald, M., Hardi, J.: HF Combustion Stability - Research Activities in Germany. Space Propulsion Conference
Schulze, M., Hummel, T., Klarmann, N., Berger, B., Schuermans, B., Sattelmayer, T.: Prediction of Linear High-Frequency Stability in Gas Turbine Combustors with Linearized Euler Equations. Journal of Engineering for Gas Turbines and Power.
Schulze, M., Fiala, T., Sattelmayer, T.: Radiation-Based Validation of Rocket Engine Simulations and Comparison to Heat Release. Journal of Propulsion and Power.
Schulze, M., Sattelmayer, T.: Numerical Study of the Influence of Absorber Rings on Acoustic Damping. Journal of Spacecraft and Rockets.
Gikadi, J., Schulze, M., Sattelmayer, T.: Petrov-Galerkin finite element schemes for the prediction of scattering matrices in ducted systems using linearized sets of equations. Aerospace Science and Technology.
A. Chemnitz, T. Sattelmayer, C. Roth, O. Haidn, Y. Daimon, R. Keller, P. Gerlinger, J. Zips., M. Pfitzner: Numerical Investigation of Flow and Combustion in a Single-Element GCH4/GOX Rocket Combustor: Aspects of Turbulence Modeling. 52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Schulze, M., Fiala, T., Sattelmayer, T.: Radiation-Based Validation of Combustion Simulations and Comparison to Heat Release in Rocket Engines. AIAA SciTech Aerospace Science Meeting
Roman Keller, Peter Gerlinger: Numerical Simulations of a Single Injector Gaseous Methane Rocket Combustion Chamber. 54th AIAA Aerospace Sciences Meeting, AIAA SciTech
Zips J., Müller H., Pfitzner M.: Non-adiabatic tabulation methods to predict wall-heat loads in rocket combustion. 36th Combustion Symposium
Stefan Gröning, Justin S. Hardi, Dmitry Suslov, Michael Oschwald: Injector-driven combustion instabilities in a hydrogen/oxygen rocket combustor. Journal of Propulsion and Power; DOI: 10.2514/1.B35768.
Stefan Gröning, Justin S. Hardi, Dmitry Suslov, Michael Oschwald: Influence of hydrogen temperature on the stability of a rocket engine combustor operated with hydrogen and oxygen. CEAS Space Journal; DOI: 10.1007/s12567-016-0130-8
W. Armbruster, S. Gröning, J. Hardi, M. Oschwald, D. Suslov: High-Frequency combustion instability with H2 injection coupling in a LOX/H2 rocket combustor. Thermoacoustic Instabilities in Gas Turbines and Rocket Engines: Industry meets Academia
J. Hardi, S. Gröning, S. Webster, S. Beinke, D. Suslov, M. Oschwald: Review of experimental test cases for modeling high frequency combustion instability. 52nd AIAA Joint Propulsion Conference
S. Gröning, J. S. Hardi, D. Suslov, M. Oschwald: Analysis of phase shift between oscillations of pressure and flame radiation intensity of self-excited combustion instabilities. 6th European Conference for Aerospace Sciences (EUCASS)
Torben Fiedler, Joachim Rösler, Martin Bäker: A Protective Coating on Copper Alloys for High Heat-Flux Applications in Rocket Engines. Materials Science and Engineering Congress
Fassin, M., Wulfinghoff, S., Reese, S.: Modelling of thermal barrier coatings and their influence on the lifetime of rocket engine nozzle structures. Proceedings of the VII European Congress on Computational Methods in Applied Sciences and Engineerin. ECCOMAS, Crete (Greece), June 5-10, 2016
Fassin, M., Kowollik, D., Reese, S., Haupt, M.: Design studies of rocket engine cooling structures for fatigue experiments. Archive of Applied Mechanics
Pasquariello, V., Hammerl, G., Örley, F., Hickel, S., Danowski, C., Popp, A., Wall, W.A., Adams, N.A.: A cut-cell finite volume – finite element coupling approach for fluid–structure interaction in compressible flow. Journal of Computational Physics.
Vito Pasquariello, Stefan Hickel, Nikolaus A. Adams: Large-Eddy Simulation of Strong Shock-Wave/Turbulent Boundary-Layer Interaction at Re_theta = 14000. 24th International Congress of Theoretical and Applied Mechanics
Vito Pasquariello, Stefan Hickel, Nikolaus A. Adams: Unsteady Effects of Strong Shock-Wave/Boundary-Layer Interaction at High Reynolds Number. Journal of Fluid Mechanics
Vito Pasquariello, Felix Örley, Stefan Hickel, Nikolaus A. Adams: Cut-Element Immersed Boundary Method for Moving Geometries and Fluid-Structure Interaction. Joint Annual Meeting of DVM and Gamm 2016
Thomas Kaller, Vito Pasquariello, Stefan Hickel, Nikolaus A. Adams: Large-Eddy Simulation of a High Reynolds Number Flow Through a High Aspect Ratio Cooling Duct. 10th International Symposium on Turbulence and Shear Flow Phenomena
Silvestri, S., Celano, M.P., Kirchberger, C., Schlieben, G., Haidn, O.J., Knab, O.: Investigation on Recess Variation of a Shear Coax Injector for a Single Element GOX/GCH4 Combustion Chamber. Transactions of the JSASS, Aerospace Technology Japan
Riedmann, H.; Görgen, J.; Ivancic, B.; Makowka, K.; Frey, M.: Numerical Simulation of the Hot Gas Side Flow and Wall Heat Transfer in CH4/Ow Rocket Thrust Chambers. Space Propulsion
Simona Silvestri, Maria Palma Celano, Gregor Schlieben, Oliver Knab, Oskar J. Haidn: Characterization of a Multi-Injector GOX-GCH4 Combustion Chamber. AIAA Joint Propulsion Conference
Simona Silvestri, Maria Palma Celano, Gregor Schlieben, Oliver Knab, Oskar J. Haidn: Experimental Investigation on Recess Variation of a Shear Coax Injector in a GOX-GCH4 Combustion Chamber. Space Propulsion
D. Schneider, C. Génin: Numerical Investigation of Flow Transition Behavior in Cold Flow Dual-Bell Rocket Nozzles. Journal of Propulsion and Power.
R. Stark, C. Génin, D. Schneider, C.M. Fromm: Ariane 5 Performance Optimization Using Dual-Bell Nozzle Extension. Journal of Spacecraft and Rockets.
Schneider, D., Génin, C., Karl, S., Hannemann, V.: A Numerical Model for Nozzle Flow Application under LOX/CH4 Hot Flow Conditions. 52nd AIAA/SAE/ASEE Joint Propulsion Conference

2015

Gerhard, N.; Iacono, F.; May, G.; Müller, S.; Schäfer, R.: A High-Order Discontinuous Galerkin Discretization with Multiwavelet-Based Grid Adaptation for Compressible Flows. Journal of Scientific Computing, 62(1), 25-52, 2015, DOI: 10.1007/s10915-014-9846-9"
Brix, K.; Campos Pinto, M.; Canuto, C., Dahmen, W.: Multilevel Preconditioning of Discontinuous-Galerkin Spectral Element Methods, Part I: Geometrically Conforming Meshes. IMA J Numer Anal(2014) ; 35 (4), 1487-1532, 2015; doi: 10.1093/imanum/dru053
Deolmi, G., Dahmen, W., Müller, S.: Effective boundary conditions for compressible flows over rough surfaces. Mathematical Models and Methods in Applied Sciences; 25(7), 1257--1297, 2015, doi:10.1142/S0218202515500323
Dahmen, W.; König, V.; Müller, S.; Rom, M.: Numerical investigation of transpiration cooling effects on turbulent boundary layers. 6th Eucass - European Conference for Aerospace Sciences - Krakow, Poland, 29 June - 03 July 2015.
W. Dahmen, S. Müller, M.Rom, S. Schweikert, M. Selzer, J. von Wolfersdorf: Numerical boundary layer investigations of transpiration-cooled turbulent channel flow. International Journal of Heat and Mass Transfer; 86, 90--100, DOI: 10.1016/j.ijheatmasstransfer.2015.02.075, 2015
G. Yahiaoui, H. Olivier: Development of a Short-Duration Rocket Nozzle Flow Simulation Facility. AIAA J. DOI: 10.2514/1.J053790.
Förner, Kilian, Cárdenas Miranda, Alejandro, Polifke, Wolfgang: Mapping the Influence of Acoustic Resonators on Rocket Engine Combustion Stability. Journal of Propulsion and Power
Kilian Förner, Wolfgang Polifke: Aero-Acoustic Characterization of Helmholtz Resonators in the Linear Regime with System Identification. 22nd International Congress on Sound and Vibration (ICSV22)"
Kilian Förner, Muttalip Akın Temiz, Wolfgang Polifke, Ines Lopez Arteaga, Avraham Hirschberg: On the Non-Linear Influence of the Edge Geometry on Vortex Shedding in Helmholtz Resonators. 22nd International Congress on Sound and Vibration (ICSV22)
Christian Dittert, Markus Selzer, Hannah Böhrk: Characterization of the Flow Field of Anisotropic Porous Cones with Different Wall Thickness. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Statnikov, V., Saile, D., Meiß, J.-H., Henckels, A., Meinke, M., Gülhan, A., Schröder, W.: Experimental and numerical investigation of the turbulent wake flow of a generic space launcher configuration. Progress in Flight Physics (7): 329–350, 2015
Saile, D., Kirchheck, D., Gülhan, A., D. Banuti: Design of a Hot Plume Interaction Facility at DLR Cologne. 8th European Symposium on Aerothermodynamics for Space Vehicles, Lisbon, Portugal, 2-6 March 2015.
Saile, D., Kirchheck, D., Gülhan, A., Serhan, C., V. Hannemann: Design of a GH2/GOX Combustion Chamber for the Hot Plume Interaction Experiments at DLR Cologne. 8th European Symposium on Aerothermodynamics for Space Vehicles, Lisbon, Portugal, 2-6 March 2015.
Scharnowski, S., Statnikov, V., Meinke, M., Schröder, W., Kähler, K.: Combined experimental and numerical investigation of a transonic space launcher wake. Progress in Flight Physics (7): 311–328, DOI : 10.1051/eucass/201507311.
Statnikov, V., Sayadi, T., Meinke, M., Schmid, P., Schröder, W.: Analysis of pressure perturbation sources on a generic space launcher after-body in supersonic flow using zonal RANS/LES and dynamic mode decomposition. Phys. Fluids, vol. 27, no. 1 (016103), pp. 1–22, 2015
Statnikov, V., Saile, D., Meiß, J.-H., Henckels, A., Meinke, M., Gülhan, A., Schröder, W.: Experimental and numerical investigation of the turbulent wake flow of a generic space launcher configuration. Progress in Flight Physics (7): 329–350, 2015
Scharnowski, S., Statnikov, V., Meinke, M., Schröder, W., Kähler, C. J.: Combined experimental and numerical investigation of a transonic space launcher wake. Progress in Flight Physics (7): 311–328, 2015
Statnikov, V., Bolgar, I., Scharnowski, S., Meinke, M., Kähler, C. J., Schröder, W.: Analysis of characteristic wake flow modes on a generic planar transonic space launcher configuration. In 6th European Conference for Aeronautics and Space Sciences (EUCASS), Krakow, 2015.
Stanikov, V., Stephan, S., Pausch, K., Meinke, M., Radespiel, R., Schröder, W.: Experimental and numerical investigations of the turbulent wake flow of a generic space launcher at M∞=3 and M∞=6. In 6th European Conference for Aeronautics and Space Sciences (EUCASS), Krakow, 2015.
Stanikov, V., Stephan, S., Pausch, K., Meinke, M., Radespiel, R., Schröder, W.: Experimental and numerical investigations of the turbulent wake flow of a generic space launcher at M∞=3 and M∞=6. CEAS Space Journal
Jie Wu, Rolf Radespiel: Experimental investigation of a newly designed supersonic wind tunnel. Progress in Flight Physics 7, pp 123-144, DOI: 10.1051/eucass/201507123
S. Stephan, J. Wu, R. Radespiel: Propulsive Jet Influence on Generic Launcher Base Flow. CEAS Space Journal; DOI:10.1007/s12567-015-0098-9
A.-M. Schreyer, S. Stephan, R. Radespiel: CHARACTERIZATION OF THE SUPERSONIC WAKE OF A GENERIC SPACE LAUNCHER. 64. Deutscher Luft- und Raumfahrtkongress,Rostock, 22. - 24. September, 2015
P. Scholz, R. Bernegger, S. Stephan: Estimation of Abberation for PIV Measurements in Compressible Flows by Means of Ray Tracing. In 6th European Conference for Aeronautics and Space Sciences (EUCASS), Krakow, 2015.
Stanikov, V., Stephan, S., Pausch, K., Meinke, M., Radespiel, R., Schröder, W.: Experimental and numerical investigations of the turbulent wake flow of a generic space launcher at M∞=3 and M∞=6. In 6th European Conference for Aeronautics and Space Sciences (EUCASS), Krakow, 2015.
SCHREYER, A. M., STEPHAN, S., RADESPIEL, R.: Characterization of the supersonic wake of a generic space launcher. Deutscher Luft- und Raumfahrtkongress
H. Lüdeke, J.D. Mulot, K. Hannemann: Launch Vehicle Base Flow Analysis Using Improved Delayed Detached Eddy Simulation. AIAA Journal, Vol. 53(9) DOI: 10.2514/1.J053297
B. Ivancic, H. Riedmann, M. Frey, O. Knab, S. Karl, K. Hannemann: Investigation of different modeling approaches for CFD simulation of high pressure rocket combustors. EUCASS Book Series Advances in Aerospace Sciences: Progress in Propulsion Physics Volume 5
Scharnowski, S.; Statnikov, V.; M.Meinke; Schröder, W. & Kähler, C.J.: Combined numerical and experimental investigation of a high subsonic space launcher wake. Progress in Flight Physics (7): 311–328, DOI : 10.1051/eucass/201507311.
S. Scharnowski, V. Statnikov, M. Meinke, W. Schröder, Ch. J. Kähler: COMBINED EXPERIMENTAL AND NUMERICAL INVESTIGATION OF A TRANSONIC SPACE LAUNCHER WAKE. EUCASS-PROGRESS IN FLIGHT PHYSICS
Sven Scharnowski, Istvan Bolgar, Christian J. Kähler:Control of the recirculation region of a transonic backward-facing step flow using circular lobes. 9th Int. Symp. on Turbulence and Shear Flow Phenomena (TSFP-9)
H. Müller, J. Matheis, S. Hickel, M. Pfitzner: Large-Eddy Simulation of Coaxial LN2/GH2 Injection at Supercritical Pressures. 53rd AIAA Aerospace Sciences Meeting, Kissimee, Florida, USA, 2014
J. Matheis, H. Müller, M. Pfitzner, S. Hickel: Large-Eddy Simulation of Coaxial LN2/GH2 Injection at Supercritical Pressures. 9th International Symposium on Turbulence and Shear Flow Phenomena (TSFP-9) June 30 - July 3, 2015, The University of Melbourne, Australia
H. Müller, C.A. Niedermeier, M. Jarczyk, M. Pfitzner, S. Hickel, N.A. Adams: Large-Eddy Simulation of Trans- and Supercritical Injection. EUCASS Book Series, Progress in propulsion physics, Vol. 8
M. Pfitzner, H. Müller: Simulation of high-pressure turbulent mixing and reacting real gas flows. 15th International Conference on Numerical Combustion, April 2015, Avignon, France
Müller H., Pfitzner M.: Large-Eddy Simulation of transcritical LOx/CH4 Jet Flames. 6th European Conference for Aeronautics and Space Sciences, July 2015, Krakow, Poland
Müller H., Pfitzner M.: Large Eddy Simulation turbulenter, nicht-vorgemischter Verbrennung unter Verwendung der Eulerian Stochastic Fields Methode in OpenFOAM. 27. VDI Flammentag, September 2015, Clausthal
Pohl S., Müller H., Pfitzner M.: Numerische Simulation der turbulenten, nicht-vorgemischten Verbrennung mit Flamelet Generated Manifolds (FGM) in OpenFOAM. 27. VDI Flammentag, September 2015, Clausthal
Müller H., Niedermeier C.A., Matheis J., Pfitzner M., Hickel S.: Large-Eddy Simulation of Nitrogen Injection at Trans- and Supercritical Conditions. Physics of Fluids
Müller H., Pfitzner M., Matheis J., Hickel S.: Large-Eddy Simulation of Coaxial LN2/GH2 Injection at Trans- and Supercritical Conditions. Journal of Propulsion and Power; DOI: 10.2514/1.B35827.
J. Matheis, H. Müller, C. Lenz, M. Pfitzner, S. Hickel: Volume translation methods for real-gas computational fluid dynamics simulations. Journal of Supercritical Fluids, doi:10.1016/j.supflu.2015.10.004
H. Müller, M. Pfitzner: Large-Eddy Simulation of transcritical LOx/CH4 Jet Flames. EUCASS book series, Progress in Propulsion Physics
Schulze, M., Sattelmayer, T.: Eigenvalue Analysis for the Prediction of Initial Growth Rates of Thermoacoustic Instability in Rocket Motors. 53rd AIAA Aerospace Sciences Meeting
Sattelmayer, T., Schmid, M., Schulze, M.: Interaction of Combustion with Transverse Velocity Fluctuations in Liquid Rocket Engines. Journal of Propulsion and Power
Sattelmayer, T., Kathan, R., Köglmeier, S., Kaess, R., Nicole, A.: Validation of Transverse Instability Damping Computations for Rocket Engines. Journal of Propulsion and Power
Schulze, M., Sattelmayer, T.: A Comparison of Time and Frequency Domain Descriptions of High Frequency Acoustics in Rocket Engines with Focus on Dome Coupling. Journal of Aerospace Science and Technology, 45, 165-177
Schulze, M., Wagner, M., Sattelmayer, T.: Linearized Euler Equations for the Determination of Scattering Matrices for Orifice and Perforated Plate Configurations in the High Mach Number Regime. International Journal of Acoustics and Vibration
Sattelmayer, T., Schmid, M., Schulze, M.: Impact of Massflow Fluctuations on Combustion Dynamics in Liquid Engines. Journal of Spacecraft and Rockets, 52(5)
Schulze, M., Kathan, R., Sattelmayer, T.: Impact of Absorber Ring Position and Cavity Length on Acoustic Damping. Journal of Spacecraft and Rockets
Hummel, T., Schulze, M., Schuermans, B., Sattelmayer, T.: Reduced Order Modeling of Transversal and Non-Compact Combustion Dynamics. 22nd International Congress of Sound and Vibration
Boger, Markus; Jaegle, F.; Klein, R., Munz, C.D.: Coupling of compressible and incompressible flow regions using the multiple pressure varaibles approach Title of Journal: "Mathematical Methods in the Applied Sciences Volume 38, pp. 458–477
F. J. Förster, S. Baab, G. Lamanna, B. Weigand: Temperature and velocity determination of shock-heated flows with non-resonant heterodyne laser- induced thermal acoustics. Applied Physics B, DOI: 10.1007/s00340-015-6217-7
Grazia. Lamanna, F. Weckenmann, S. Baab, B. Weigand , H. Fulge, S. Fasoulas, J. Steelant: Reconstruction of the local temperature distribution from integral thermographic data. Optics Communications
G. Lamanna, P. Rack, Y. Khanfir, H. Fulge, S. Fasoulas, G. Gréhan, S. Saengkaew, B. Weigand, J. Steelant: Droplet sizing and infrared temperature measurements in superheated sprays. Proc. of the 8th European Symposium onAerothermodynamics for Space Vehicles
Lempke, M., Gerlinger, P., Seidl, M.S., Aigner, M.: Unsteady High-Order Simulation of a Liquid Oxygen/Gaseous Hydrogen Rocket Combustor. Journal of Propulsion and Power, doi: 10.2514/1.B35726.
Keller R., Gerlinger P.: Numerical Simulations of a gaseous Methane Rocket Model Combustion Chamber. 6th European Conference for Aeronautics and Space Sciences (EUCASS), Krakow (2015)
Lempke M., Keller R., Gerlinger P.: Influence of Spatial Discretization and Unsteadiness on the Simulation of Rocket Combustors. International Journal for Numerical Methods in Fluids, 79, 437-455, DOI: 10.1002/fld.4059"
Matheis, J., Müller, H., Pfitzer, M., Hickel, S.: Volume translation methods for real-gas computational fluid dynamics simulations. Journal of Supercritical Fluids. doi: 10.1016/ j.supflu.2015.10.004.
Pohl, S., Frank, G., M. Pfitzner: Heat Transfer in Reacting Cooling Films: Influence and Validation of Combustion Modeling in Numerical Simulations. ASME Journal of Turbomachinery 137(8). 081003-081003-10
Frank, G. and Pfitzner, M.: Numerical Study of Reactive Boundary Layers on Transpiration Cooled Surfaces. 6th European Conference for Aeronautics and Space Sciences (EUCASS), Krakow, Poland, 2015
G. Frank, M. Pfitzner: On the generation of non-adiabatic, nonpremixed flamelet libraries with special emphasis on wall heat losses. MCS-2015: Ninth Mediterranean Combustion Symposium
G. Frank, M. Pfitzner: Numerical Study of Wall Heat Fluxes in Reactive Boundary Layers on Transpiration Cooled Surfaces. EUCASS 2015, 6th European Conference for Aeronautics and Space Sciences, Krakow 2015
Pohl, S.; G. Frank; M. Pfitzner: Heat Transfer in Reacting Cooling Films: Influence and Validation of Combustion Modeling in Numerical Simulations. Journal of Turbomachinery
Lorenz Boeck, Thomas Fiala, Josef Hasslberger, Thomas Sattelmayer: Application of High-Speed OH-PLIF to DDT Experiments. 25th International Colloquium on the Dynamics of Explosions and Reactive Systems (ICDERS), Leeds, UK, August 2-8, 2015
Thomas Fiala, Thomas Sattelmayer: Heat Release and UV-VIS Radiation in Non-Premixed Hydrogen-Oxygen Flames. Experiments in Fluids; DOI: 10.1007/s00348-015-2013-8
Thomas Fiala, Thomas Sattelmayer: Assessment of Existing and New Modeling Strategies for the Simulation of OH* Radiation in High-Temperature Flames. CEAS Space Journal; DOI: 10.1007/s12567-015-0107-z
Thomas Fiala, Thomas Sattelmayer: Modeling of the Continuous (Blue) Radiation in Hydrogen Flames. Journal of Hydrogen Energy
Torben Fiedler, Joachim Rösler, Martin Bäker: Development of a CuNiCrAl Bond-Coat for Thermal Barrier Coatings in Rocket Combustion-Chambers. Journal of Thermal Spray Technology; DOI:10.1007/s11666-015-0325-0
Torben Fiedler, Martin Bäker, Joachim Rösler: Finite Element Simulation of Thermal Barrier Coatings in Rocket Engines. SIMULIA Community Conference Proceedings, pp. 207-218
T. Fiedler, J. Schloesser, J. Rösler, M. Bäker: Development of a thermal-barrier coating-system for rocket combustion chambers. European Conference for Aerospace Sciences
Martin Bäker, Torben Fiedler, Joachim Rösler: Stress evolution in thermal barrier coatings for rocket engine applications. Mechanics of Advanced Materials and Modern Processes. DOI: 10.1186/s40759-015-0005-2
Kowollik, Daniel; Lindhorst, Klemens; Haupt, Matthias; Horst, Peter. Surrogate Model Framework for Transient Coupled Thermal Analyses. Computational Mechanics
M. Fassin, S. Wulfinghoff, S. Reese: Application of an elastoplastic material model coupled with anisotropic damage for the failure prediction of a rocket combustion chamber wall. EUCASS 2015
S. Wulfinghoff, M. Fassin, S. Reese: Strictly increasing anisotropic damage. International Journal of Damage Mechanics
M. Fassin, S. Wulfinghoff, S. Reese: Different Numerical Time Integration Schemes for Elastoplasticity Coupled to Anisotropic Damage. Applied Mechanics and Materials
S. Wulfinghoff, M. Fassin, S. Reese: Comparison of Two Time-Integration Algorithms for an Anisotropic Damage Model coupled to Plasticity. Applied Mechanics and Materials
R. G. Thiede, E. B. Zametaev, J. Riccius, M. Fassin, S. Reese: Comparison of damage parameter based finite element fatigue life analysis results to combustion chamber type TMF panel test results. 51th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
M. Fassin, D. S. C. Kowollik, S. Reese, M. Haupt: Design studies for rocket engine cooling structures for fatigue experiments. Archive of Applied Mechanics
M.C. Haupt, D. S. C. Kowollik, K. Lindhorst, F. Hötte: Fluid-Structure-Interaction in Rocket Thrust Chambers - Simulation and Validation. International Conference on Advanced Computational Engineering and Experimenting, ACE-X
D.S.C. Kowollik, M. Haupt, P. Horst: Transient Fluid-Structure Interaction Analysis of a Cooled Rocket Thrust Chamber Based on Three Coupling Domains. 5th European Conference for Aeronautics and Space Sciences, EUCASS 2013, Number ISBN: 978-84-941531-0-5
Wulfinghoff,S., Reese,S., Fassin,M., Kiliclar,Y., Brepols,T., Rezaei,S.: Properties and Restrictions related to Anisotropic Damage Theories based on 2nd Order Damage Tensors. Proceedings of the 3rd ECCOMAS Young Investigators Conference on Computational Methods in Applied Sciences and 6th GACM Colloquium on Computational Mechanics
Vuong, Yoshihara, Wall: A general approach for modeling porous flow structure interaction under finite deformations. Computer Methods in Applied Mechanics and Engineering, 283, 1240 - 1259
Felix Örley, Vito Pasquariello, Stefan Hickel, Nikolaus A. Adams: Cut-element based immersed boundary method for moving geometries in compressible liquid flows with cavitation. Journal of Computational Physics
Vito Pasquariello, Georg Hammerl, Felix Örley, Stefan Hickel, Caroline Danowski, Alexander Popp, Wolfgang A. Wall, Nikolaus A. Adams: A cut-cell Finite Volume - Finite Element coupling approach for fluid-structure interaction in compressible flow. Journal of Computational Physics
Pasquariello, V., Hickel, S., Adams, N.A., Hammerl, G., Wall, W.A., Daub, D., Willems, S., Gülhan, A.: Coupled simulation of shock-wave/turbulent boundary-layer interaction over a flexible panel. 6th European Conference For Aerospace Sciences
Dennis Daub, Sebastian Willems, Ali Gülhan: Experimental Results on Shock-Wave / Boundary-Layer Interaction induced by a Movable Wedge. 8th European Symposium on Aerothermodynamics
Dennis Daub, Sebastian Willems, Ali Gülhan: Experimental results on unsteady shock-wave/boundary-layer interaction induced by an impinging shock. CEAS Space Journal
D. Daub, S. Willems, A. Gülhan: Experiments on the Interaction of a Fast-Moving Shock with an Elastic Panel. AIAA Journal
Sebastian Willems, Burkard Esser, Ali Gülhan: Experimental and numerical investigation on thermal fluid–structure interaction on ceramic plates in high enthalpy flow. CEAS Space Journal; DOI10.1007/s12567-015-0101-5
F. Breede, D. Koch, E. Maillet, G. N. Morscher: Modal acoustic emission of damage accumulation in C/C–SiC composites with different fiber architectures. Ceramics International
F. Breede, S. Hofmann, N. Jain, R. Jemmali, D. Koch, H. Voggenreiter: Design, manufacture and characterization of a carbon fiber reinforced silicon carbide nozzle extension. Journal of Applied Ceramic Technology
H. Rochlitz, P. Scholz: Cooling channel flow characterization using Particle Image Velocimetry and Laser Induced Fluorescence. CEAS 2015
H. Rochlitz, P. Scholz: Application of Particle Image Velocimetry and Laser Induced Fluorescence in a cooling channel flow. AIAA Aviation Conferecne - Summer 2015
Henrik Rochlitz , Peter Scholz, Thomas Fuchs: The flow field in a high aspect ratio cooling duct with and without one heated wall. Experiments in Fluids, Volume 56, Issue 12, DOI: 10.1007/s00348-015-2071-y
Slavinskaya, N.A., Abbasi, A., Weinschenk, M., Haidn, O.J.: Methane Skeletal Mechanism for Space Propulsion Applications. 5th Int. Workshop on Model Reduction in Reacting Flows
Celano, M.P., Silvestri, S., Perakis, N, Schily, F., Celano, M.P., Haidn, O.J.: Heat Flux Evaluation Methods for a Single Element Heat Sink Chamber. 6th European Conference on Aeronautics and Space Science
Celano, M.P., Silvestri, S., Kirchberger, C., Schlieben, G., Suslov, D., Haidn, O.J.: Gaseous Film Cooling Investigation and Model Assessment in a Sub-scale Single Element GOX/GCH4 Combustion Chamber. 30th Int. Symposium on Space technology and Science
Celano, M.P., Silvestri, S., Schlieben, G., Kirchberger, C., Haidn, O.J.: Injector Characterization for a GOX-GCH4 Single Element Combustion Chamber. EUCASS Advances in Aerospace Sciences, Progress in Propulsion Physics Vol. 9"
Hoeglauer, Kniesner, Knab, Schlieben, Kirchberger, Silvestri, Haidn: Modeling and Simulation of a GOX/Kerosene Subscale Rocket Combustion Chamber with Film Cooling. CEAS Space Journal; DOI:10.1007/s12567-015-0096-y"
Knab, Aichner, Frey, Hoeglauer, Ivancic, Kniesner, Riedmann: Consequences of Modeling Demands on Numerical Rocket Thrust Chamber Flow Simulation Tools. EUCASS 2015
Riedmann, Banuti, Ivancic, Knab, Hannemann: Modeling of H2/O2 Single-Element Rocket Thrust Chamber Combustion at Sub- and Supercritical Pressures with Different CFD Tools. EUCASS 2015
Silvestri, S., Celano, M.P., Haidn, O.J., Knab, O.: Comparison of Single Element Rocket Combustion Chambers with Round an Square Cross Sections. 6th European Conference for Aeronautics and Space Sciences
Silvestri, S., Celano, M.P., Kirchberger, C., Schlieben, G., Haidn, O.J., Knab, O.: Investigation on Recess Variation of a Shear Coax Injector for a Single Element GOX/GCH4 Combustion Chamber. 30th Int. Symposium on Space Technology and Science
Génin C., Stark R., Jack, S.: Flow separation in out-of-round nozzles, a numerical and experimental study. EUCASS Flight physics Books, Vol. 7
Génin, C., Jack, S., Stark, R.: Flow visualization in out-of-round rocket nozzles. 30th International Symposium on Shock Waves (ISSW30)
Schneider, D., Génin, C.: Numerical Investigation of Flow Transition Behavior in Cold Flow Dual Bell Rocket Nozzles. 51st AIAA Joint Propulsion Conference
Génin, C., Jack, S.: Flow separation study in stiff ovalized rocket nozzles, Part I: Experimental approach. 51st AIAA Joint Propulsion Conference
Genin, C., Schneider, D., Takahashi, H. , Tomita, T.: LOX/CH4 Hot Firing Dual Bell Nozzle Testing: Part I -Transitional Behavior. 51st AIAA Joint Propulsion Conference

2014

Gerhard, Nils; Müller, Siegfried: Adaptive multiresolution Discontinuous Galerkin Schemes for Conservation Laws: Multi-dimensional case. Computational and Applied Mathematics, 35(2), 321-349, 2016, DOI:10.1007/s40314-014-0134-y, 2014
Dahmen, Wolfgang; Plesken, Christian; Welper, Gerrit: Double Greedy Algorithms: Reduced Basis Methods for Transport Dominated Problems. ESAIM: Mathematical Modelling and Numerical Analysis, 48(3), 623–663, 2014.
Dahmen, W.; Gotzen, T. S.Mueller, Michael Rom: Numerical simulation of transpiration cooling through porous material. International Journal for Numerical Methods in Fluids, 76(6), 331–365, 2014. DOI: 10.1002/fld.3935
Dahmen, W., Gerber, V., Gotzen, Th., Müller, S., Rom, M., Windisch, Ch.: Numerical Simulation of transpiration cooling with a mixture of thermally perfect gases. ECCOMAS 2014, 20 - 25 July 2014, Barcelona
M.A. Keller, M.J. Kloker, H. Olivier: Influence of Cooling-Gas Properties on Film-Cooling Effectiveness in Supersonic Flow. Journal of Spacecraft and Rockets 52 (5), 1443-1455; doi: http:// arc.aiaa.org/doi/abs/10.2514/1.A33203.
Cárdenas Miranda, A., Polifke, W: Combustion Stability Analysis of Rocket Engines with Resonators Based on Nyquist Plots. Journal of Propulsion and Power
Keller M.A., Kloker M.J.: Study of Flow Control by Localized Volume Heating in Hypersonic Boundary Layers. CEAS Space Journal
Keller M.A., Kloker M.J.: Effusion cooling and flow tripping in laminar supersonic boundary-layer flow. AIAA-Journal
Keller, M.A., Kloker, M.J., Olivier, H.: Influence of Cooling-Gas Properties on Film-Cooling Effectiveness in Supersonic Flow. Journal of Spacecraft and Rockets
Herbertz, A., Selzer, M.: Analysis of Coolant Mass Flow Requirements for Transpiration Cooled Ceramic Thrust Chambers. Transaction of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan
Saile, D., A. Gülhan: Plume-Induced Effects on the Near-Wake Region of a Generic Space Launcher Geometry. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, 16-20 June 2014.
Statnikov, V., Sayadi, T., Meinke, M., Schmid, P., Schröder, W.: Investigations of unsteady transonic and supersonic wake flow of generic space launcher configurations using zonal RANS/LES and dynamic mode decomposition. High Performance Computing in Science and Engineering’14 (eds.: Nagel, W. E., Kröner, D. H., and Resch, M. M.), Springer, pp. 379–402, 2014.
Statnikov, V., Sayadi, T., Meinke, M., Schröder, W., Schmid, P.: On the source of pressure perturbations on the after-body of space launchers via zonal RANS-LES and Dynamic Mode Decomposition. Ercoftac ETMM 10, Marbella, Spain, 2014.
Marcus Casper, Sören Stephan, Peter Scholz, Rolf Radespiel: Qualification of oil-based tracer particles for heated Ludwieg tubes. Experiments in Fluids; DOI: 10.1007/s00348-014-1753-1
Jie Wu, Rolf Radespie, Pradip Zamre: Disturbance characterization and flow quality improvement in a Tandem Nozzle Mach 3 Wind Tunnel. Experiments in Fluids; DOI: 10.1007/s00348-014-1887-1
K. Oßwald, A. Siegmund, P. Birken, V. Hannemann, A. Meister: L²Roe: A low-dissipation version of Roes approximate Riemann solver for low Mach numbers. International Journal for Numerical Methods in Fluids
S. Scharnowski, C. J. Kähler: Investigation of a transonic separating/reattaching shear layer by means of PIV. Theoretical and Applied Mechanical Letters
Keppeler R., Tangermann E., Pfitzner, M.: LES of low to high turbulent combustion in an elevated pressure environment. Flow, Turbulence, and Combustion, Ausgabe 03/2014, 767-802
H. Müller, M. Pfitzner: Large-Eddy Simulation of Coaxial LN2/GH2 Injection at Supercritical Pressures. 9th International OpenFOAM Workshop, 23-26 June, 2013, Zagreb, Croatia (2014)
Schulze, M., Sattelmayer, T.: Low-Order Modelling of the Non-Local Acoustic Reacting Combustion Chamber-Dome Interface in Rocket Engines. 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Schulze, M., Urbano, A., Zahn, M., Schmid, M., Sattelmayer, T., Oschwald, M.: Thermoacoustic Feedback Analysis of a Cylindrical Combustion Chamber under Supercritical Conditions. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Ohio, Cleveland
Schulze, M., Sattelmayer, T.: Frequency Domain Simulations for the Determination of Liner Effects on Longitudinal Wave Propagation. International Journal of Aeroacoustics, 14(7)
Schulze, M., Morgenweck, D., Sattelmayer, T.: About Flame-Acoustic Coupling Phenomena in Supercritical H2/O2 Rocket Combustion Systems. Deutscher Luft- und Raumfahrtkongress
Schulze, M., Urbano, A., Zahn, M., Schmid, M., Sattelmayer, T., Oschwald, M.: Thermoacoustic Feedback Analysis of a Cylindrical Combustion Chamber under Supercritical Conditions. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Schulze, M., Sattelmayer, T.: Low-Order Modelling of the Non-Local Acoustic Reacting Combustion Chamber-Dome Interface in Rocket Engines: 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Boger, M.; Jaegle, F.; Weigang, B., Munz, C.-D.: A pressure-based treatment for the direct numerical simulation of compressible multi-phase flow using multiple pressure variables. Computers and Fluids, Vol. 96, pp. 338-349
S. Baab, G. Lamanna, B. Weigand: Combined Elastic Light Scattering and Two-Scale Shadowgraphy of Near-Critical Fuel Jets. ILASS Americas 26th Annual Conference on Liquid Atomization and Spray Systems
Lempke M., Gerlinger P., Seidl M., Aigner M.: Time-Accurate High-Order Numerical Simulation of a Subcritical LOX-H2 Single Element Rocket Combustor. Journal of Propulsion and Power
Frank G., Pohl S., Pfitzner M.: Heat transfer in reacting cooling films, part II: Modelling near-wall effects in non-premixed combustion with OpenFOAM. ASME Turbo Expo 2014, GT2014-25215
Pohl S., Frank G., Pfitzner M.: Heat transfer in reacting cooling films, part I: Influence and validation of combustion modelling in CFD simulations. ASME Turbo Expo 2014, GT2014-25220
Thomas Fiala, Thomas Sattelmayer: Non-Premixed Counterflow Flames: Scaling Rules for Batch Simulations. Journal of Combustion
Thomas Fiala, Michael Nettinger, Franz Rieger, Abhijeet Kumar, Thomas Sattelmayer: Emission and Absorption Measurement in Enclosed Round Jet Flames. 16th International Symposium on Flow Visualization
Gröning, S.; Suslov, D.; Hardi, J., Oschwald, M.: Influence of hydrogen temperature on the acoustics of a rocket engine combustion chamber operated with LOX/H2 at representative conditions. Space Propulsion 2014
T. Fiedler, T. Fedorova, J. Rösler, M. Bäker: Design of a Nickel-Based Bond-Coat Alloy for Thermal Barrier Coatings on Copper Substrates. Metals, 4, 503-518
M. Fassin, V. Tini, I. Vladimirov, S. Reese: Lifetime prediction of a rocket combustion chamber wall by a viscoplastic damage model. Proceedings in Applied Mathematics and Mechanics; Wiley; 2014
I.N. Vladimirov, M.P. Pietryga, Y. Kiliclar, V. Tini, S. Reese: Failure modelling in metal forming by means of an anisotropic hyperelastic-plasticity model with damage. International Journal of Damage Mechanics, SAGE publications; 2014; ISSN: 1056-7895
K. Lindhorst, M. C. Haupt, P.Horst: Efficient Surrogate Modelling of Nonlinear Aerodynamics in Aerostructural Coupling Schemes. AIAA Journal, 52, 1952-1966
Yoshihara, Coroneo, Comerford, Bauer, Klöppel, Wall: A combined fluid-structure interaction and multi-field scalar transport model for simulating mass transport in biomechanics. Numerical Methods in Engineering, Volume 100, Issue 4 , Pages 277–299
Ehrl, A., Popp, A., Gravemeier, V., Wall, W.A.: A dual mortar approach for mesh tying within a variational multiscale method for incompressible flow Title of Journal: Int. Journal for Numerical Methods in Fluids, Volume 76, Issue 1 Pages 1–27
Schott, B.; Wall, W.A.: A new face-oriented stabilized XFEM approach for 3D incompressible Navier-Stokes equations. Computer Methods in Applied Mechanics and Engineering Volume 276, 1 July 2014, Pages 233–265
Coroneo, Yoshihara, Wall: Biofilm growth: a multi-scale and coupled fluid-structure interaction and mass transport approach. Biotechnology and Bioengineering, Volume 111, Issue 7 Pages 1385–1395
Vito Pasquariello, Muzio Grilli, Stefan Hickel, Nikolaus A. Adams: Large-eddy simulation of passive shock-wave/boundary-layer interaction control. International Journal of Heat and Fluid Flow.
Felix Örley, Vito Pasquariello, Stefan Hickel, Nikolaus A. Adams: Cut-element based immersed boundary method for moving geometries in compressible liquid flows with cavitation. Journal of Computational Physics, 283, 1–22. http://doi.org/10.1016/j.jcp.2014.11.028
Castiglioni, G., Domaradzki, J.A., Pasquariello, V., Hickel, S., Grilli, M.: Numerical simulations of separated flows at moderate Reynolds numbers appropriate for turbine blades and unmanned aero vehicles. International Journal of Heat and Fluid Flow
M. P. Celano, S. Silvestri, G. Schlieben, C. Kirchberger, O. J. Haidn, S. Menon: Numerical and experimental investigation for a GOX-GCH4 shear-coaxial injector element. Space Propulsion 2014, 19th to 22nd May 2014, Cologne, Germany
H. Rochlitz, P. Scholz: Wärmeübergangs-Versuche an einer generischen Kühlkanalgeometrie. 63. Deutscher Luft- und Raumfahrtkongress, Augsburg, 2014
M. P. Celano, S. Silvestri, G. Schlieben, C. Kirchberger, O. J. Haidn, S. Menon: Numerical and experimental investigation for a GOX-GCH4. Space Propulsion 2014
S. Silvestri, M. P. Celano, G. Schlieben, C. Kirchberger, O. J. Haidn: Characterization of a GOX-GCH4 Single Element Combustion Chamber. Space Propulsion 2014, 19th to 22nd May 2014, Cologne, Germany
C. Höglauer, B. Kniesner, O. Knab, G. Schlieben, O.J. Haidn: Validation of cooling film modellling in rocket combustion chambers. Space Propulsion 2014, 19th to 22nd May 2014, Cologne, Germany
G. Schlieben, C. Kirchberger, O.J. Haidn, C. Höglauer, B. Kniesner, O. Knab: Experimental and Numerical Film Cooling Investigations in a GOX/Kerosene Rocket Combustion Chamber. AIAA-2014-4008, AIAA Propulsion and Energy 2014
Riedmann, Kniesner, Frey, Munz: 3D Modeling of Spray Combustion and Flow in a 40kN H2/O2 Subscale Rocket Thrust Chamber. Space Propulsion 2014
Génin, C., Stark, R.: Optimierung von Dual-Bell-Düsenerweiterungen. 61. Deutscher Luft- und Raumfahrt Kongress.
Schneider, D., Génin, C., Stark, R., Fromm C.: Ariane 5 performance optimization using dual bell nozzle extension. 4th Space Propulsion Conference

2013

Hombsch, M.; Olivier, H.: Film Cooling in Laminar and Turbulent Supersonic Flows. Journal of Spacecraft and Rockets 50:742-753
Cárdenas Miranda, A., Polifke, W.: On the Reflection, Transmission, Coupling and Damping of Non-Plane Acoustic Modes by Resonator Rings. 5th European Conference for Aeronautics and Space Sciences (EUCASS), München 2013
Keller, Michael; Kloker, M.J.: DNS of Effusion Cooling in a Supersonic Boundary-Layer Flow: Influence of Turbulence. AIAA-2013-2897
Groskopf, G., Kloker M. J.: Effects of an Oblique Roughness on Hypersonic Boundary-Layer Transition. In: High Perfomance Computing in Science and Engineering 12 (eds. M.M. Resch & al.), Springer
Keller, M.A.; Kloker, M.J.: DNS of Film Cooling in a Supersonic Boundary-Layer Flow on Massively-Parallel Supercomputers. Sustained Simulation Performance 2013 (eds. M.M. Resch & al.), Springer
Ortelt, M., Hald, H., Herbertz, A., Müller, I.:Advanced Design Concepts for Ceramic Thrust Chamber Components of Rocket Engines. 5th European conference for aeronautics and space sciences
Herbertz, Armin, Selzer, Markus: Analysis of Coolant Mass Flow Requirements for Transpiration Cooled Ceramic Thrust Chambers. 29th International Symposium on Space Technology and Science
Herbertz, A., Ortelt, M., Müller, I., Hald, H.: C*-Effciency Evaluation of Transpiration Cooled Ceramic Combustion Chambers. 4th CEAS Air & Space Conference
S. Schweikert, J. von Wolfersdorf, M. Selzer, H. Hald: Characterization of Actively Cooled Porous C/C Wall Segments According to Pressure Loss and Internal Temperature Distribution. Proceedings of the 7th EuropeanWorkshop on Thermal Protection Systems & Hot Structures
Ortelt, M., Breede, F., Herbertz, A., Koch, D., Hald, H.: Current activities in the field of ceramic based rocket engines. ODAS Symposium
S. Schweikert, J. von Wolfersdorf, M. Selzer, H. Hald: Experimental Investigation of Velocity and Temperature Distributions in Turbulent Cross Flows over Transpiration Cooled C/C Wall Segments. 5TH European Conference for Aeronatics and Space Sciences.
Selzer, Markus, Schweikert, Sven, Hald, Hermann, von Wolfersdorf, Jens: Transfer of an analytical transpiration cooling model to the cooling analysis of rocket combustion chambers made of ceramic matrix composites. 5th European conference for aeronautics and space sciences (Eucass)
Saile, D., Gülhan, A., Henckels, A.: Investigations on a Backward-Facing Step by Means of a Microphone Array and IR-Thermography. 5th European Conference for Aeronautics and Space Sciences, Munich, Germany, 1-5 July
Saile, D.; Gülhan, A.; Henckels, A.; Glatzer, C.; Statnikov, V.; Meinke, M.: Investigations on the turbulent wake of a generic space launcher geometry in the hypersonic flow regime. EUCASS Progress in Flight Physics Volume 5, pp. 209-234, DOI: 10.1051/eucass/201305209
Statnikov, V., Sayadi, T., Meinke, M., Schröder, W., Schmid, P.: Dynamic mode decomposition of supersonic and transonic wakes of generic space launcher configurations. In 66th Annual Meeting of the APS Division of Fluid Dynamics, Pittsburgh, 2013
Statnikov, V., Saile, D., Meiß, J.-H., Henckels, A., Meinke, M., Gülhan, A., Schröder, W.: Experimental and Numerical Investigation of the Turbulent Wake Flow of a Generic Space Launcher Configuration. Progress in Flight Physics (7): 329–350.
Statnikov, V., Meiß, J.-H., Meinke, M., Schröder, W.: Investigation of the Turbulent Wake Flow of Generic Launcher Configurations via a Zonal RANS/LES Method. CEAS Space Journal, DOI: 10.1007/s12567-013-0045-6, 5(1-2):75–86, 2013
Statnikov, V., Glatzer, C., Meiß, J.-H., Meinke, M., Schröder, W.: Numerical investigation of the near wake of generic space launcher systems at transonic and supersonic flows. Progress in Flight Physics (5): 191–208, 2013
Saile, D., Gülhan, A., Henckels, A., Glatzer, C., Statnikov, V., Meinke, M.: Investigations on the turbulent wake of a generic space launcher geometry in the hypersonic flow regime. Progress in Flight Physics (5): 209–234, 2013
Jie Wu, Rolf Radespiel: Tandem nozzle supersonic wind tunnel design. International Journal of Engineering Systems Modelling and Simulation (IJESMS), Vol. 5, No. 1/2/3, 2013
S. Stephan, R. Radespiel, R. Müller-Eigner: Jet Simulation Facility using the Ludwieg Tube Principle. 5th EUCASS. July 2013, Munich
Kai Oßwald, Volker Hannemann, Klaus Hannemann, Sören Stephan, Rolf Radespiel: Numerical and Experimental Investigations of a Generic Rocket Launcher Configuration with Cold Plume in Hypersonic Flow. 5th European Conference for Aeronautics and Space Sciences (EUCASS)
Wolf, C., You, Y., Hörnschemeyer, R., Lüdecke, H., Hannemann, V.: Base-flow sensitivity of a generic rocket forbody towards small freestream angles. Progress in Flight Physics Eucass Book Series, 5 (6). p.169-190
Scharnowski, S., Kähler, C.J.: Bestimmung höherer Momente mittels Ensemble-Korrelationsauswertung. Fachtagung "Lasermethoden in der Strömungsmesstechnik", Munich, Germany, September 3-5
Cierpka, C.; Scharnowski, S.; Ehlert, M.; Manhart, M., Kähler, C.J.: Characterization of the flow over periodic hills with advanced measurement and evaluation techniques. 8th Int. Symp. on Turbulence and Shear Flow Phenomena (TSFP 8), Poiters, France, August 28-30
Huisman, S.G.; Scharnowski, S.; Cierpka, C.; Kähler, C. J.; Lohse, D.; Sun, Ch.: Direct experimental measurement of logarithmic boundary layers in highly turbulent Taylor-Couette flow. Physical Review Letters
Kähler, C.J.; Cierpka, C., Scharnowski, S.: High resolution velocity profile measurements in turbulent boundary layers. 8th Int. Symp. on Turbulence and Shear Flow Phenomena (TSFP 8), Poiters, France, August 28-30
Scharnowski, S., Kähler, C.J.: Investigation of a transonic axisymmetric backward facing step flow by means of high resolution PIV. 8th Int. Symp. on Turbulence and Shear Flow Phenomena (TSFP 8), Poiters, France, August 28-30
Scharnowski, S., Kähler, C.J.: Methods for estimating higher order moments from PIV data. 10th International Symposium on Particle Image Velocimetry PIV13, Delft, The Netherlands, July 1-3
Cierpka, C.; Scharnowski, S.; Manhart, M. & Kähler, C.J.: On the significance of high spatial resolution to capture all relevant scales in the turbulent flow over periodic hills. 10th International Symposium on Particle Image Velocimetry PIV13, Delft, The Netherlands, July 1-3
Cierpka, C., Scharnowski S., Kähler C.J.: Parallax correction for precise near-wall flow investigations. Applied Optics
C.A. Niedermeier, S. Hickel, N.A. Adams "Assessment of Implicit Subgrid-Scale Modeling for Turbulent Supercritical Mixing. Proceedings of the Ercoftac Workshop Direct and Large-Eddy Simulation 9, Dresden, Germany, April 3-5, 2013
Jarczyk M., Pohl S., Müller H., Pfitzner, M.: CFD-Simulation of LOX/H2 injection, mixing and combustion at supercritical pressures. ERCOFTAC Bulletin 96 - Reactive Flows and Combustion (2013)
Pohl S., Jarczyk M., Pfitzner M., Rogg B.: Real gas CFD simulations of hydrogen/oxygen supercritical combustion. EUCASS Book Series, Progress in Propulsion Physics Vol. 4
Ferraro F., Pfitzner, M.: Hybrid LES-RANS transported PDF method for non-premixed methane/air flames using different chemistry mechanisms. 6th European combustion meeting, 25-28 June 2013, Lund, Sweden (2013)
H. Müller, C.A. Niedermeier, M. Jarczyk, M. Pfitzner, S. Hickel, N.A. Adams: Large-Eddy Simulation of Trans- and Supercritical Injection. 5th European Conference for Aeronautics and Space Sciences (EUCASS), Munich, 2013
Müller H., Ferraro F., Pfitzner, M.: Implementation of a Steady Laminar Flamelet Model for nonpremixed combustion in LES and RANS simulations. 8th International OpenFOAM Workshop, June 11-14, 2013, JeJu, Korea (2013)
Müller H., Pfitzner M.:Numerical Computation of Real Gas CH4/O2 Counterflow Diffusion Flames using OpenFOAM. OSCIC12: Open Source CFD International Conference, October 29-30 2012, London, UK (2012)
C.A. Niedermeier, H. Müller, M. Jarczyk, S. Hickel, N.A. Adams, M. Pfitzner: Large-Eddy Simulation of Turbulent Trans- and Supercritical Mixing. 21st AIAA Computational Fluid Dynamics Conference, AIAA Paper 2013-2950, DOI: 10.2514/6.2013-2950
Schulze, M., Schmid, M., Morgenweck, D., Kögelmeier, S., Sattelmayer, T.: A Conceptional Approach for the Prediction of Thermoacoustic Stability in Rocket Engines. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, California, USA, 2013
Schulze, M., Gikadi, J., Sattelmayer, T.: Acoustic Admittance Prediction of Two Nozzle Designs of Different Length Using Frequency Domain Simulations. 5th European Conference for Aeronautics and Space Sciences, Munich, Germany, 2013
Wagner, M., Schulze, M., Sattelmayer, T.: Experimental Investigation of Acoustic Properties of Orifices s and Perforated Plates in the High Mach Number Regime. Proceedings of the ICSV, 2013
Schmid, M., Blumenthal, R.S., Schulze, M., Polifke, W., Sattelmayer, T.: Quantitative Stability Analysis Using Real-Valued Frequency Response Data. Journal of Engineering for Gas Turbines and Power, Vol. 135, No. 1, pages 121601, 2013
Lamanna, G.; Kamoun, H.; Arnold, B.; Schlottke, K.; Weigand, B.; Steelant, J.: Differential infrared thermography (DIT) in a flashing jet: a feasibility study Quantitative InfraRed Thermography Journal, vol. 10 (1), pp. 112-131
Oldenhof, E.; Weckenmann, F.; Lamanna, G.; Weigand, B.; Bork, B.; Dreizler, A.: Experimental investigation of isolated acetone droplets at ambient and near-critical conditions, injected in a nitrogen atmosphere. Progress in Propulsion Physics, Vol. 4, pp. 257-270
Lempke, M.; Gerlinger, P.; Aigner, M.: Assumed PDF Modeling in Rocket Combustor Simulations. Progress in Propulsion Physics, Vol. 4, 2013, pp. 569-582
G. Frank, H. Müller, M. Pfitzner: Implementierung eines Flamelet-Modells für nicht vorgemischte Verbrennung in OpenFOAM. 26. Deutscher Flammentag
Jan Matheis, Bernd Budich, Stefan Hickel: Large Eddy Simulation of the Transition Process from Regular to Irregular Shock-Wave/Boundary-Layer Interaction. Eighth International Symposium on Turbulence and Shear Flow Phenomena (TSFP8)
Frank G., Ferraro, F., Pfitzner, M.: RANS simulations of reacting cooling films. 5th European Conference for Aeronautics and Space Sciences (EUCASS), Munich (2013)
Pohl, S., Jarczyk, M., Pfitzner, M., B. Rogg: Real gas CFD simulations of hydrogen/oxygen supercritical combustion. Progress in Propulsion Physics 4, 583-614
T. Fiala, T. Sattelmayer: A Posteriori Computation of OH∗ Radiation from Numerical Simulations in Rocket Combustion Chambers. European Conference for Aeronautics and Space Sciences (EUCASS)
T. Fiala, T. Sattelmayer: Heat Release and OH* Radiation in Laminar Non-Premixed Hydrogen-Oxygen Flames. 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Number 2013-1170, dx.doi.org/10.2514/6.2013-1170  
T. Fiala, T. Sattelmayer: Non-Premixed Counterflow Flame Simulations: Scaling Rules for Fast Batch Simulations European Combustion Meeting 2013
T. Fiala, T. Sattelmayer: On the Use of OH* Radiation as a Marker for the Heat Release Rate in High-Pressure Hydrogen-Oxygen Liquid Rocket Combustion. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Number 2013-3780, http://dx.doi.org/10.2514/6.2013-3780
S. Gröning, D. Suslov, M. Oschwald, T. Sattelmayer: Stability Behaviour of a Cylindrical Rocket Engine Combustion Chamber OperatedWith Liquid Hydrogen and Liquid Oxygen. 5th European Conference for Aeronautics and Space Sciences (EUCASS), Munich, Germany, 1-5 July 2013
Gröning, S.; Oschwald, M., Sattelmayer, T.: Einfluss einer Kavität auf das Druckfeld der ersten tangentialen Mode einer Raketenbrennkammer unter repräsentativen Bedingungen. 62. Deutscher Luft- und Raumfahrtkongress
D. Kowollik, V.Tini, S. Reese, M. Haupt: 3D fluid–structure interaction analysis of a typical liquid rocket engine cycle based on a novel viscoplastic damage model. International Journal for Numerical Methods in Engineering
D.S.C. Kowollik, M.C. Haupt, P. Horst: Mesh Deformation with Exact Surface Reconstruction Using a Reduced Radial Basis Function Approach. V International Conference on Computational Methods for Coupled Problems in Science and Engineering
Schott, B.; Massing, A.; Wall, W. A.: A face-oriented stabilized fictitious domain approach for 3D incompressible Navier-Stokes equations applied to fluid-structure interaction26th Nordic Seminar on Computational Mechanics, Oslo, Norway, October 2013
Danowski, C., Gravemeier, V., Yoshihara, L., Wall, W.A.: A monolithic computational approach to thermo-structure interaction. International Journal for Numerical Methods in Engineering
Popp, Gee, Wall: A primal-dual active set strategy for finite deformation dual mortar contact. CMIS’ Conference issue, Series: Lecture Notes in Applied and Computational Mechanics, Springer 2013, 56, 151-171
Popp, Seitz, Gee, Wall: Improved robustness and consistency of 3D contact algorithms basedon a dual mortar approach. Computer Methods in Applied Mechanics and Engineering
Vito Pasquariello, Jan Matheis, Muzio Grilli, Stefan Hickel: Large-Eddy Simulation of Passive Shock-Wave / Boundary-Layer Interaction Control. Eighth International Symposium on Turbulence and Shear Flow Phenomena (TSFP8)
Popp, Gee, Wall: Mortar methods for single- and multi-field applications in computational mechanics. In: High Performance Computing on Vector Systems 2012, M. Resch et al. (Eds.), Springer, 2013, 133-154
Willems, S., Gülhan, A., Esser, B.: Shock induced fluid structure interaction on a flexible wall in supersonic turbulent flow. Progress in Flight Physics, Vol. 5, 285-308, EDP Sciences, 2013
Breede, F.; Jemmali, R.; Koch , D., Voggenreiter, H: Design and testing of a C/C-SiC nozzle extension manufactured via filament winding technique and liquid silicon infiltration. Ceramic Transactions
M. P. Celano, S. Silvestri, G. Schlieben, C. Kirchberger, O. J. Haidn: Injector Characterization for a GOX-GCH4 Single Element Combustion Chamber. 5th European Conference for Aeronautics and Space Sciences (EUCASS), Munich, Germany, 1-5 July 2013
Slavinskaya, N.A., Wiegand, M.A., Starcke, J.H., Riedel, U., Haidn, O.J.: Kinetic Mechanism for Low-Pressure Methane/Air Combustion. EUCASS Advances in Aerospace Sciences, Progress in Propulsion Physics Vol. 4
C. Kirchberger, G. Schlieben, O.J. Haidn: Assessment of Film Cooling Characteristics in a GOX/ Kerosene Rocket Combustion Chamber. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Jose, CA, USA, 15-17 July 2013
C. Bauer, G. Schlieben, O.J. Haidn. Design and Commission of a mobile GOX/CH4 rocket combustion test bed for education and collegiate research. 29th International Symposium on Space Technology and Science, Nagoya-Aichi, Japan, 2-9 June 2013
C. Kirchberger, G. Schlieben, O.J. Haidn: Investigation on Film Cooling in a GOX/ Kerosene Rocket Combustion Chamber. 29th International Symposium on Space Technology and Science, Nagoya-Aichi, Japan, 2-9 June 2013
C. Höglauer, B. Kniesner, O. Knab, G. Schlieben, O.J. Haidn: Simulation of liquid, transcritical and gaseous cooling films5th European Conference for Aeronautics and Space Sciences (EUCASS), Munich, Germany, 1-5 July 2013
M. P. Celano, S. Silvestri, G. Schlieben, C. Kirchberger, O.J. Haidn: Injector Characterization for a GOX-GCH4 Single Element Combustion Chamber. EUCASS Advances in Aerospace Sciences, Progress in Propulsion Physics Vol. 7
Kirchberger, C., Schlieben, G., Haidn, O.J.: Investigation on Film Cooling in a GOX/ Kerosene Rocket Combustion Chamber. 29th Int. Symposium on Space Technology and Science
Génin, C., Gernot, A., Stark, R.: Experimental and Numerical Study of Heat Flux in Dual Bell Nozzles. Journal of Propulsion and Power
Génin, C., Stark, R., Schneider, D.: Transitional Behavior of Dual Bell Nozzles: Contour Optimization. 49th AIAA Joint Propulsion Conference
Génin, C., Stark, R., Jack, S.: Flow separation in out-of-round nozzles, a numerical and experimental study. 5th European Conference for Aerospace Sciences
Verma, S.B., Stark, R., Haidn, O.: Reynolds number influence on dual-bell transition phenomena. Journal of Propulsion and Power, 29 (3) , pp. 602-609

2012

Groskopf, G.; Kloker, M.J.:Stability analysis of three-dimensional hypersonic boundary-layer flows with discrete surface roughness. NATO-RTO-Tagung, San Diego, NATO-RTO-MP-AVT-200-30:1-19.
Statnikov, V., Meiß, J.-H., Meinke, M., Schröder, W.: Investigation of the Turbulent Wake Flow of Generic Launcher Configurations via a Zonal RANS/LES Method. 61. Deutscher Luft- und Raumfahrtkongress, Berlin, 2012
Marcus Casper, Sören Stephan, Jan Windte, Peter Scholz, Rolf Radespiel: Hypersonic PIV in a Ludwieg Tube Wind Tunnel at Mach 5.9. 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference, 25-28 June 2012, New Orleans, Louisiana
M. Casper, S. Stephan, P. Scholz and R. Radespiel: Particle Image Velocimetry at a Generic Space Launcher Model at Mach 5.9.16th Int Symp on Applications of Laser Techniques to Fluid Mechanics Lisbon, Portugal, 09-12 July, 2012
S. Stephan, R. Radespiel, R. Müller-Eigner: Propulsive Jet Simulation in a Hypersonic Ludwieg Tunnel. 61. Deutscher Luft- und Raumfahrtkongress
Y. You, K. Oßwald, H. Lüdeke, V. Hannemann: Numerical Study of the Subsonic Base Flow with a Side Support. Progress in Hybrid RANS-LES Modelling, Springer Verlag, Vol. 117, pp. 427-437
Scharnowski, S., Kähler, C.J.:Analyse der transsonischen Heckströmung im Nachlauf eines generischen Raketenmodells mit PIV. 18. DGLR-Fachsymposium der STAB, Stuttgart, Germany, November 6-7
Cierpka, C.; Scharnowski, S.; Ehlert, M.; Manhart, M., Kähler, C.J.:High resolution flow field measurements around periodic hills. 18. DGLR-Fachsymposium der STAB, Stuttgart, Germany, November 6-7
Casper, M.; Stephan, S.; Windte, J.; Scholz, P.; Radespiel, R.; Scharnowski, S., Kähler, C.J.: Hypersonic PIV in a Ludwieg Tube Wind Tunnel at Mach 5.9.28th AIAA Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference, New Orleans, Louisiana, USA, 25-28 June
Kähler, C.J.; Scharnowski, S., Cierpka, C.:Near-wall resolution of turbulent boundary layers. 9th European Fluid Mechanics Conference, Rome, Italy, September 9-13
Kähler, C.J.; Scharnowski, S., Cierpka, C.: Near-wall resolution of turbulent boundary layers. Fachtagung Lasermethoden in der Strömungsmesstechnik, Rostock, Germany, September 6-8
Scharnowski, S.; Kähler C. J.: On the effect of curved streamlines on the accuracy of PIV vector fields. Experiments in Fluids
Kähler, C.J.; Scharnowski, S., Cierpka, C.: On the resolution limit and uncertainty of DPIV and PTV near walls. 18. DGLR-Fachsymposium der STAB, Stuttgart, Germany, November 6-7
Kähler, C.J.; Scharnowski, S., Cierpka, C.. On the resolution limit of digital particle image velocimetry. Experiments in Fluids, 52, 1629 - 1639
Kähler, C.J.; Scharnowski, S., Cierpka, C.: On the uncertainty of digital PIV and PTV near walls. Experiments in Fluids, 52, 1641 - 1656
Scharnowski, S.; Hain, R. & Kähler, C.J.: Reynolds stress estimation up to single-pixel resolution using PIV-measurements. Experiments in Fluids, 52, 985-1002
Scharnowski, S., Kähler, C.J.: Third-order accurate digital particle image velocimetry. 16th International Symposium on Applications of Laser techniques to Fluid Mechanics, Lisbon, Portugal, July 9-12
Schulze, M.; Morgenweck, D.; Sattelmayer, T.:Dämpfung akustischer Wellen durch Absorber in Raketentriebwerken. Deutscher Luft- und Raumfahrtkongress, Berlin, Germany, 2012
M. Boger, F. Jaegle, S. Fechter, C.-D. Munz: A Pressure-Based Method for the Direct Numerical Simulation of Compressible Two-Phase Flows. 12th Triennial International Conference on Liquid Atomization and Spray Systems (ICLASS)
Boger, M., Jaegle, F., Fechter, S., Weigand, B., Munz, C.-D.: Direct numerical simulation of compressible multi-phase flow with a pressure-based method. 7th International Conference on Computational Fluid Dynamics (ICCFD7)
Grazia Lamanna, Ernst Oldenhof, Steffen Baab, Ingo Stotz, Bernhard Weigand: Disintegration Regimes Near the Critical Point. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference
Gröning, S.; Oschwald, M., Sattelmayer, T.: Selbst erregte tangentiale Moden in einer Raketenbrennkammer unter repräsentativen Bedingungen. 61. Deutscher Luft- und Raumfahrtkongress
Danowski, Yoshihara, Wall: A monoltithic computational approach to thermo-structure interaction. Proceedings ECCOMAS Special Interest Conference - Numerical Heat Transfer 2012, Wroclaw, Poland, September 2012, 419-420
Hammerl, Danowski, Grilli, Adams, Wall: A thermo-fluid-structure interaction approach based on an immersed interface method and on a monolithic thermo-structure interaction approach. YIC2012 - European Community on Computational Methods in Applied Sciences Young Investigators Conference, Aveiro, Portugal, April 24 - April 27, 2012, Seite 142
Grilli, Hickel, Adams, Hammerl, Danowski, Wall: An innovative approach to thermo-fluid-structure interaction based on an immersed interface method and a monolithic thermo-structure interaction algorithm. 42nd AIAA Fluid Dynamics Conference and Exhibit, New Orleans, USA Juni 2012, AIAA paper 2012-3267
Yoshihara, Bauer, Comerford, Coroneo, Klöppel, Vuong, Wall: Multi-scale computational modeling of coupled mass transfer and tissue deformation in biomechanics. ECCOMAS Special Interest Conference-Numerical Heat Transfer, 4-6- Sept. 2012, Gliwice-Wroclaw, Poland, 21-22
Breede, F.; Friess, M.; Koch, D., Jemmali, R.: Mechanical and Microstructural Characterization of C/C-SiC Manufactured Via Triaxial and Biaxial Braided Fiber Preforms. Ceramic Engineering and Science Proceedings, Volume 33 Issue 2
Schlieben, G., Kirchberger, C., Haidn, O.J.: Using Intra-Cooling Channel Measurements for Film Cooling Investigations in a GOX/Kerosene Rocket Combustion Chamber. AIAA Joint Propulsion Conference
Kirchberger, C., Schlieben, G., Haidn, O.J.: Assessment of Analytical Models for Film Cooling in a Hydro-Carbon/GOX Rocket Combustion Chamber . AIAA Joint Propulsion Conference
Génin C., Stark, R.: Influence of the test environment on the transition of dual-bell nozzles. 28th ISTS Special Issue, Vol. 10, pp 49-53
Génin C., Stark R., Haidn O., Quering K., Fey, M.: Experimental and Numerical Study of Dual Bell Nozzle Flow. EUCASS Flight Physics Book Vol. 5
Génin C., Stark R., Karl S. & Schneider D.: Numerical Investigation of Dual Bell Nozzle Flow Field. 48th AIAA Joint Propulsion Conference

2011

Saile, D.; Gülhan, A.; Glatzer, C.; Meiß, J.-H.; Meinke, M.; Schröder, W.: Experimental and Numerical Investigations on the Turbulent Wake of a Generic Space Launcher Geometry in the Hypersonic Flow Regime. 4th European Conference for Aerospace Sciences (EUCASS), St. Petersburg, Russia
Saile, D.; Gülhan, A.; Henckels, A.: Investigations on the Near-Wake Region of a Generic Space Launcher Geometry. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, California
Morgenweck, D., Sattelmayer, T., Fassl, F., Kaess, R.: Influence of Scaling Rules on Loss of Acoustic Energy. Journal of Spacecraft and Rockets
Breede, F.; Hofmann, S.; Klatt, E.; Denis, S.: Influence of Fiber Orientation on the Mechanical Properties and Microstructure of C/C-SiC Composite Plates Produced by Wet Filament Winding Technique, Processing and Properties of Advanced Ceramics and Composites III, Volume 225
Génin, C., Stark, R.: Side Loads in Subscale Dual Bell Nozzles. Journal of Propulsion and Power
Génin C., Stark R.: Hot flow testing of dual bell nozzle. 49th Aerospace Science Meeting
Stark, R., Génin, C.: Influence of the test environment on the transition of dual-bell nozzles. 28th International Symposium on Space Technology and Science (ISTS)
Genin C.; Stark R.; Haidn O.; Quering K., Frey M.: Experimental and Numerical Study of Dual Bell Nozzle Flow. 4th European Conference for Aerospace Sciences
Génin C., Stark R.: Experimental investigation of the inflection geometry on dual bell nozzle flow behavior. 47th AIAA Joint Propulsion Conference
Génin C., Gernoth A., Stark R.:Experimental and numerical study of heat flux in dual bell nozzles. 47th AIAA Joint Propulsion Conference

2010

Génin, C., Stark, R.: Experimental Study on Flow Transition in Dual Bell Nozzles. Journal of Propulsion and Power
Stark R., Nürnberger-Génin C.: Side Loads in Dual Bell Nozzles,Part I: Phenomenology. 46th AIAA Joint Propulsion Conference
Nürnberger-Génin C., Stark R.: Side Loads in Dual Bell Nozzles,Part II: Design Parameters. 46th AIAA Joint Propulsion Conference

2009

Nürnberger-Génin C., Stark R.: Experimental Study on Flow transition in Dual Bell Nozzles. 45th AIAA Joint Propulsion Conference

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Lehrstuhl für Aerodynamik und Strömungsmechanik

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