Final Colloquium SFB TRR40

Records

Fundamental Numerical and Experimental Investigations of Transpiration Cooling with Rocket Science Applications.

Numerical and Experimental Investigation on Film Cooling in Supersonic Flows

Heat Transfer in Pulsating Flow and its Impact on Temperature Distribution and Damping Performance of Acoustic Resonators

Interactions of axisymmetric Dual-Bell nozzles with external flows

Disintegration regimes and mixing at near critical conditions: an experimental and numerical study

High-order numerical simulations of rocket combustion chambers using ideal and real gas equations

Heat transfer in nozzle cooling channels

Direct numerical simulation of a hypersonic boundary layer with porous wall injection

Design and fundamental studies of Dual-Bell nozzles

Definition and Evaluation of Advanced Rocket Thrust Chamber Concept

Recent Progress in Combustion and Heat Transfer Modeling in LOX/Methane Rocket Combustion Chambers

Lifetime of Thrust Chambers: Experiment, Prediction and Thermal Barrier Coatings

SFB-TRR40 Final Colloquium Lectures

Experimental and Numerical Study of High-Frequency Combustion Instabilities

Thermomechanical Fluid-Structure Interaction in Supersonic Flows: Experiments and Simulation

Requirements Towards Predictive Simulations of Combustion in Rocket Motors

COUPLED THERMAL AND STRUCTURAL OPTIMIZATION OF A METAL-OR CFRP-BASED CRYOGENIC PROPULSION STAGE

Hot Plume Impact on Rocket Base Flows

Direct numerical simulation of a hypersonic boundary layer with porous wall injection