ANALYSIS OF FILM COOLING AND HEAT TRANSFER IN ROCKET THRUST CHAMBER AND NOZZLE
49th, Aerospace sciences meeting; 49th AIAA Aerospace Sciences meeting including the New Horizons Forum and Aerospace Exposition 2011 ; 2011 ; Orlando, FL
01.01.2011
14 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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NTIS | 1965
|Rocket engine thrust chamber heat transfer calculation and analysis (Final rept.)
Tema Archiv | 1974
|NTRS | 1965
|