Computations of axisymmetric plug-nozzle flowfields: Flow structures and thrust performance

Journal of Propulsion and Power

Volumn 18, Issue 2, 2002, Pages 254-260

  Ito, Takashi ^a   Fujii, Kozo ^a   Hayashi, A Koich ^a  

^a UNIVERSITY OF TOKYO   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; NOZZLES; PRESSURE DISTRIBUTION; PRESSURE EFFECTS; PROPULSION; SHOCK WAVES;

PLUG NOZZLE FLOWFIELDS; THRUST PERFORMANCE;

ROCKETS;

EID: 0036493957     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5964     Document Type: Article

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