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Technische Universität München

Projekt DFG BR1511-6

Effect of modulated leading-edge pulsed blowing on the delta-wing post-stall flow field. © Andrei Buzica
Phase-averaged PIV crossflow planes of the manipulated flowfield with synchronized pulsating jets. © Andrei Buzica
Massive separation above a delta wing during post-stall at AoA = 45°. DFG BR1511-6. © Andrei Buzica
Pulsed blowing at the leading-edge reattaches the separated shear layer at AoA = 45°. DFG BR1511-6. © Andrei Buzica

Projekt DFG BR1511-9

Blunt leading-edge separation characteristic and vortex development: turbulent vs. transitional flow. © Andrei Buzica
Separation characteristic and leading-edge vortex development above the AVT-183 diamond-wing. Research project DFG BR1511-9. © Andrei Buzica
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