Computational investigation of flow through a louvered inlet configuration
Author:
Affiliation:
1. Middle East Technical Univ., Ankara, Turkey
2. U.S. Naval Postgraduate School, Monterey, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2477
Reference4 articles.
1. Tuncer I.H. and Platzer M.F., A Computational Study of Subsonic Flow Over A Close-Coupled Delta Canard-Wing-Body Configuration) AIAA Journal of Aircraft, Vol.35, No.4 July-August 1998, pp.554-560
2. Navier-Stokes Analysis of Subsonic Flowfields over a Missile Configuration
3. Numerical investigation of subsonic flow over a typical missile forebody
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1. Computational Investigation of Flow Through a Louvered Inlet Configuration;Journal of Aircraft;2002-09
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