Numerical investigations of HSCT inlet unstart transient at angle of attack

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Zha, Ge Cheng ^a   Knight, Doyle D ^b   Smith, Donald ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b RUTGERS UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW OF FLUIDS; NAVIER STOKES EQUATIONS; PROPULSION; TURBULENCE MODELS;

BALDWIN-LOMAX ALGEBRAIC TURBULENCE MODELS; COMPUTED FLOWS; HIGH SPEED CIVIL TRANSPORTS; MIXED COMPRESSIONS; NAVIER-STOKES SOLVER; NUMERICAL INVESTIGATIONS; SHOCK/BOUNDARY LAYER INTERACTIONS; TIME-ACCURATE;

ANGLE OF ATTACK;

EID: 84963787959     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-3583     Document Type: Conference Paper

References (23)

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