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

被引:0
|
作者
Boelens, O.J. [1 ,9 ]
Badcock, K.J. [2 ,10 ]
Görtz, S. [3 ,11 ]
Morton, S. [4 ,12 ]
Fritz, W. [5 ,13 ]
Karman Jr., S.L. [6 ,14 ]
Michal, T. [7 ]
Lamar, J.E. [8 ,15 ]
机构
[1] National Aerospace Laboratory, NLR, 1006 BM Amsterdam, Netherlands
[2] University of Liverpool, Liverpool, L69 7BZ, United Kingdom
[3] Royal Institute of Technology, 100 44 Stockholm, Sweden
[4] U.S. Air Force, Eglin Air Force Base, FL 32542, United States
[5] European Aeronautic Defence and Space Company, 81633 Munich, Germany
[6] University of Tennessee at Chattanooga, Chattanooga, TN 37403, United States
[7] Boeing Company, St. Louis, MO 63166-0516, United States
[8] NASA Langley Research Center, Hampton, VA 23681-2199, United States
[9] Applied Computational Fluid Dynamics, Department of Flight Physics and Loads, Aerospace Vehicles Division, P.O. Box 90502, Netherlands
[10] Department of Engineering, Computational Fluid Dynamics Laboratory, United Kingdom
[11] DLR, German Aerospace Center, Lilienthalplatz 7, 38108 Braunschweig, Germany
[12] Seek Eagle Office, 205 West D Avenue, United States
[13] Aerodynamics and Methods, Unit OPEA31
[14] Graduate School of Computational Engineering, United States
[15] Configuration Aerodynamics Branch, Mail Stop 499, United States
来源
Journal of Aircraft | 2009年 / 46卷 / 02期
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摘要
Journal article (JA)
引用
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页码:369 / 376
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