F16-XL Geometry and Computational Grids Used in Cranked-Arrow Wing Aerodynamics Project International-Reference-Cited by-同舟云学术

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F16-XL Geometry and Computational Grids Used in Cranked-Arrow Wing Aerodynamics Project International

Published:2009-03 Issue:2 Volume:46 Page:369-376
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Boelens O. J.¹,Badcock K. J.²,Görtz S.³,Morton S.⁴,Fritz W.⁵,Karman S. L.⁶,Michal T.⁷,Lamar J. E.⁸

Affiliation:

1. National Aerospace Laboratory/NLR, 1006 BM Amsterdam, The Netherlands

2. University of Liverpool, Liverpool, England L69 7BZ United Kingdom

3. Royal Institute of Technology, 100 44 Stockholm, Sweden

4. U.S. Air Force, Eglin Air Force Base, Florida 32542

5. European Aeronautic Defence and Space Company, 81633 Munich, Germany

6. University of Tennessee at Chattanooga, Chattanooga, Tennessee 37403

7. The Boeing Company, St. Louis, Missouri 63166-0516

8. NASA Langley Research Center, Hampton, Virginia 23681-2199

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.34852

Reference19 articles.

1. Overview of the Cranked-Arrow Wing Aerodynamics Project International

2. Comparison of Measured and Block Structured Simulation Results for the F-16XL Aircraft

3. Lessons Learned from Numerical Simulations of the F-16XL Aircraft at Flight Conditions

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