Hybrid Grid Solutions on the (CAWAPI) F-16XL Using Falcon v4-Reference-Cited by-同舟云学术

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Hybrid Grid Solutions on the (CAWAPI) F-16XL Using Falcon v4

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Davis Myron¹,Reed Christopher¹,Yagle Patrick¹

Affiliation:

1. Aerodynamics and CFD

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-680

Reference8 articles.

1. 1Lamar,J.E.,Obara,C.J.,Fisher,B.D.,andFisher,D.F."Flight,Wind-Tunnel,andComputationalFluidDynamics Comparison for Cranked Arrow Wing(F-16XL-1) at Subsonicand TransonicSpeeds", NASA/TP-2001-210629, February2001.

2. Characteristic-Based Schemes for the Euler Equations

3. 5Smith,B.R."Thek-klTurbulenceModelandWallLayerModelforCompressibleFlows,"AIAAPaper90-1483, June1990.

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