Numerical analysis and optimization of two-dimensional hypersonic inlets

AIAA Paper

Volumn , Issue , 2004, Pages 9610-9623

  Hasegawa, Susumu ^a,b,c   Knight, Doyle ^a  

^a RUTGERS UNIVERSITY   (United States)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c Numerical Space Engine Team   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AUTOMATION; BOUNDARY LAYERS; COMBUSTION CHAMBERS; HYPERSONIC FLOW; INTAKE SYSTEMS; NAVIER STOKES EQUATIONS; NUMERICAL ANALYSIS; OPTIMIZATION; PARAMETER ESTIMATION; PERTURBATION TECHNIQUES; PRESSURE EFFECTS; REYNOLDS NUMBER; SENSITIVITY ANALYSIS;

HYPERSONIC INLETS; OPTIMIZATION LOOP; PRESSURE RECOVERY; SUPERSONIC SPEEDS;

SPACE RESEARCH;

EID: 2942722644     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-856     Document Type: Conference Paper

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