Analysis of transonic flow on a slender delta wing using CFD

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 2, Issue , 2006, Pages 995-1016

  Schiavetta, L A ^a,d   Boelens, O J ^b,e   Fritz, W ^c,f  

^a UNIVERSITY OF GLASGOW   (United Kingdom)

^b NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

^c AIRBUS GROUP INNOVATIONS   (Germany)

^d Department of Aerospace Engineering   (United Kingdom)

^e Aerospace Vehicles Division

^f Department of Flight Physics ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; DELTA WING AIRCRAFT; SUBSONIC FLOW; VELOCITY MEASUREMENT; VORTEX FLOW;

COMPUTATIONAL FACTORS; VORTEX BREAKDOWN; VORTEX STRENGTHS;

TRANSONIC FLOW;

EID: 33845438089     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-3171     Document Type: Conference Paper

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