Study of the reverse delta wing

Journal of Aircraft

Volumn 48, Issue 1, 2011, Pages 277-286

  Altaf, Afaq ^a,b   Omar, Ashraf A ^a,b   Asrar, Waqar ^a,b   Jamaluddin, Hani Bin Ludin ^a,b  

^a INTERNATIONAL ISLAMIC UNIVERSITY MALAYSIA   (Malaysia)

^b Gombak ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SOFTWARE; REYNOLDS NUMBER; VELOCITY MEASUREMENT; VORTEX FLOW; WIND TUNNELS; WINGS;

AERODYNAMIC COEFFICIENTS; CHORD-BASED REYNOLDS NUMBER; COMPUTATIONAL FLUID DYNAMICS SOFTWARE; LOW-SPEED WIND TUNNEL; PARTICLE IMAGE VELOCIMETRIES; SURFACE PRESSURES; TANGENTIAL VELOCITIES; VORTEX STRUCTURES;

DELTA WING AIRCRAFT;

EID: 79551662961     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.C031101     Document Type: Article

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