Study of flow separation in truncated ideal contour nozzle

Journal of Propulsion and Power

Volumn 18, Issue 5, 2002, Pages 1112-1121

  Verma, S B ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FLOW VISUALIZATION; NOZZLES; PRESSURE DISTRIBUTION; PRESSURE MEASUREMENT; REYNOLDS NUMBER; ROCKETS;

FLOW SEPARATION; MACH NUMBER; PRESSURE RATIO; SCHLIEREN FLOW VISUALIZATION; TRUNCATED IDEAL CONTOUR NOZZLE;

FLOW OF FLUIDS;

EID: 0036747345     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.6042     Document Type: Article

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