Analysis of Film Cooling and Heat Transfer in Rocket Thrust Chamber and Nozzle
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
01.01.2011
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
ANALYSIS OF FILM COOLING AND HEAT TRANSFER IN ROCKET THRUST CHAMBER AND NOZZLE
British Library Conference Proceedings | 2011
|NTIS | 1965
|Rocket engine thrust chamber heat transfer calculation and analysis (Final rept.)
Tema Archiv | 1974
|NTRS | 1965
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