Comparison of Measured and Block Structured Simulation Results for the F-16XL Aircraft-Reference-Cited by-同舟云学术

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

Published:2009-03 Issue:2 Volume:46 Page:377-384
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,Elmilgui A.³,Abdol-Hamid K. S.⁴,Massey S. J.⁵

Affiliation:

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

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

3. Analytical Services and Materials, Inc., Hampton, Virginia 23666

4. NASA Langley Research Center, Hampton, Virginia 23681

5. Eagle Aeronautics, Hampton, Virginia 23666

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.35064

Reference16 articles.

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

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

3. Standard Unstructured Grid Solutions for Cranked Arrow Wing Aerodynamics Project International F-16XL

4. Reynolds-Averaged Navier-Stokes Solutions for the CAWAPI F-16XL Using Different Hybrid Grids

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