F-16XL geometry and computational grids used in cranked-arrow wing aerodynamics project international

Journal of Aircraft

Volumn 46, Issue 2, 2009, Pages 369-376

  Boelens, O J ^a,i   Badcock, K J ^b,j   Gortz S ^c,k   Morton, S ^d,l   Fritz, W ^e,m   Karman Jr , S L ^f,n   Michal, T ^g   Lamar, J E ^h,o  

^a NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

^b UNIVERSITY OF LIVERPOOL   (United Kingdom)

^c ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

^d USAF   (United States)

^e AIRBUS GROUP INNOVATIONS   (Germany)

^f UNIVERSITY OF TENNESSEE AT CHATTANOOGA   (United States)

^g BOEING COMPANY   (United States)

^h NASA LANGLEY RESEARCH CENTER   (United States)

ⁱ Aerospace Vehicles Division   (Netherlands)

^j Computational Fluid Dynamics Laboratory ^*  (United Kingdom)

^k GERMAN AEROSPACE CENTER DLR   (Germany)

^l Seek Eagle Office   (United States)

^m Unit OPEA31

ⁿ Graduate School of Computational Engineering   (United States)

^o Distinguished Research Associate   (United States)

more..

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL GEOMETRY; FLIGHT DYNAMICS; GRID COMPUTING; NASA; RESEARCH AIRCRAFT; SUPERSONIC AIRCRAFT; WINGS;

COMPUTATIONAL FLUID DYNAMICS METHODS; EUROPEAN AERONAUTIC DEFENCE AND SPACES; NASA LANGLEY RESEARCH CENTER; NATIONAL AEROSPACE LABORATORIES; ROYAL INSTITUTE OF TECHNOLOGY; STRUCTURED MULTIBLOCK GRIDS; U.S. AIR FORCE ACADEMIES; UNIVERSITY OF TENNESSEE;

DELTA WING AIRCRAFT;

EID: 63349091634     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.34852     Document Type: Article

References (19)

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