Unsteadiness of Flow Separation and End-Effects Regime in a Thrust-Optimized Contour Rocket Nozzle

Flow, Turbulence and Combustion

Volumn 71, Issue 1-4, 2003, Pages 161-181

  Nguyen, Anh Thi ^a   Deniau, H ^a   Girard, S ^a   Alziary De Roquefort, T ^a  

^a Laboratoire d'Etudes Aerodynamiques Poitiers   (France)

Author keywords

Free shock separation; Nozzle; Restricted shock separation; Side loads

Indexed keywords

HYSTERESIS; NOZZLES; OSCILLATIONS; PRESSURE EFFECTS; ROCKETS; STEADY FLOW; UNSTEADY FLOW;

FREE SHOCK SEPARATION (FSS); RESTRICTED SHOCK SEPARATION (RSS); SIDE LOADS;

TURBULENT FLOW;

EID: 1442286940     PISSN: 13866184     EISSN: None     Source Type: Journal    
DOI: 10.1023/B:APPL.0000014927.61427.ad     Document Type: Conference Paper

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