Determining exit conditions that result when heat is withdrawn from rocket thrust chamber and added to gas flow in nozzle
Effect of chamber-to-nozzle heat exchange on frozen and equilibrium flows in De Laval nozzles
1970-04-01
Report
No indication
English
Cryogenic Homogeneous Two-Phase Flows in Choked Laval Nozzles
British Library Conference Proceedings | 1998
|Minimum Length Axisymmetric Laval Nozzles
AIAA | 1975
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