A Coupled Two-Domain Approach for Transpiration Cooling
Calculation of the Thermoacoustic Stability of a Main Stage Thrust Chamber Demonstrator
Collaborative Research for Future Space Transportation Systems
Definition and Evaluation of Advanced Rocket Thrust Chamber Demonstrator Concepts
Disturbance Development in an Obstacle Wake in a Reacting Hypersonic Boundary Layer
Effects of a Launcher’s External Flow on a Dual-Bell Nozzle Flow
Experimental Investigation of Injection-Coupled High-Frequency Combustion Instabilities
Experiments on Aerothermal Supersonic Fluid-Structure Interaction
Film Cooling in Rocket Nozzles