A computational study of subsonic flowfields over a missile configuration-Reference-Cited by-同舟云学术

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A computational study of subsonic flowfields over a missile configuration

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Tuncer I.¹,Platzer M.¹,VanDyken R.²,Tuncer I.¹,Platzer M.¹,VanDyken R.²

Affiliation:

1. U.S. Naval Postgraduate School, Monterey, CA

2. U.S. Navy, Weapons Div., China Lake, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-635

Reference14 articles.

1. Ying, S.X., Steger, J.L., Schiff, L.B. and Baganoff, D. Numerical Simulation of Unsteady, Viscous High-Angle-of-Attack Flows Using a Partially Flux-Split Algorithm, AIAA Paper 86-2179,1986

2. A 3-D chimera grid embedding technique

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3. Computational Study of Subsonic Flow over a Delta Canard-Wing-Body Configuration;Journal of Aircraft;1998-07

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