Throttling a Laval Nozzle by a Vortex: An Analytical Theory AIAA Paper
45th, AIAA aerospace sciences meeting ; 2007 ; Reno, NV
2007-01-01
2007-1282
Papers in the range 2007 17 to 1467 with gaps. Held on CD-ROM
Aufsatz (Konferenz)
Englisch
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Engineering Index Backfile | 1949
|Inviscid Laval-nozzle flowfield calculation
AIAA | 1988
|Theory and experiment study on LAVAL nozzle applied to compound engine
Tema Archiv | 1999
|CECE: A Deep Throttling Demonstrator Cryogenic Engine for NASA's Lunar Lander AIAA Paper
British Library Conference Proceedings | 2007
|