Design of three-dimensional hypersonic inlets with rectangular-to-elliptical shape transition

Journal of Propulsion and Power

Volumn 15, Issue 3, 1999, Pages 408-416

  Smart, M K ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; HYPERSONIC FLOW; JET ENGINES; MACHINE DESIGN; PERFORMANCE; PRESSURE; SHOCK WAVES; THREE DIMENSIONAL; VISCOUS FLOW;

INVISCID STREAM TRACING TECHNIQUES; SHOCK WAVE INTERACTION; THREE DIMENSIONAL HYPERSONIC INLETS;

INTAKE SYSTEMS;

EID: 0033131888     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5459     Document Type: Article

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