Time-dependent supersonic separation of tangent bodies

Journal of Aircraft

Volumn 33, Issue 5, 1996, Pages 938-949

  Mosbarger, Neal A ^a,c   King, Paul I ^b,d  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^c Aeromechanics Division

^d NONE

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; MATHEMATICAL MODELS; SHOCK WAVES; SUPERSONIC FLOW; THREE DIMENSIONAL; WIND TUNNELS;

SUPERSONIC SEPARATION; TANGENT BODIES; TRANSIENT EFFECTS; WEDGE;

SUPERSONIC AERODYNAMICS;

EID: 0030246831     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.47039     Document Type: Article

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