Critical states and flow structure on a 65-deg delta wing

Journal of Aircraft

Volumn 33, Issue 2, 1996, Pages 347-352

  Jobe, Charles E ^a,b   Hsia, Alexander H ^a,b   Jenkins, Jerry E ^a,b   Addington, Gregory A ^a,b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AERODYNAMICS; DELTA WING AIRCRAFT; FLIGHT DYNAMICS; FLOW OF FLUIDS; LIFT; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; NUMERICAL METHODS; SPEED; VORTEX FLOW;

ANGLE OF ATTACK; CRITICAL STATES; FLOW STRUCTURE; FLOW TOPOLOGY; NONLINEAR INDICIAL RESPONSE;

WINGS;

EID: 0030109752     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.46944     Document Type: Article

References (16)

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