Scalability for rocket nozzle flows based on subscale and full-scale testing

Journal of Propulsion and Power

Volumn 19, Issue 3, 2003, Pages 321-331

  Hagemann, Gerald ^a   Alting, Jan ^a   Preclik, Dieter ^a  

^a AIRBUS DEFENCE AND SPACE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW PATTERNS; MATHEMATICAL MODELS; NOZZLES; PROPULSION;

FLOW SEPARATION; ROCKET NOZZLES; ROCKET PROPULSION;

ROCKET ENGINES;

EID: 0037842801     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.6123     Document Type: Article

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