Validation of Supersonic Film Cooling Modeling for Liquid Rocket Nozzle Applications
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
01.01.2010
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
FILM COOLING MODELING IN LIQUID ROCKET THRUST CHAMBERS
TIBKAT | 2021
|Film cooling modeling in liquid rocket thrust chambers
AIAA | 2021
|Liquid propellant rocket engine nozzle with passive condensate cooling
Europäisches Patentamt | 2021
|Liquid Metal Heat Pipes for Cooling Rocket Nozzle Walls
AIAA | 2003
|