Numerical investigation of subsonic flow over a typical missile forebody-Reference-Cited by-同舟云学术

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Numerical investigation of subsonic flow over a typical missile forebody

Published:1996-01-15 Issue: Volume: Page:
ISSN:
Container-title:34th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Tuncer Ismail¹,Marvin Ron¹,Platzer Max¹

Affiliation:

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

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-189

Reference17 articles.

1. Numerical simulation of vortex unsteadiness on slender bodies of revolution at large incidence

2. A numerical study of three-dimensional separated flow past a hemisphere cylinder

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Computational investigation of flow through a louvered inlet configuration;19th AIAA Applied Aerodynamics Conference;2001-06-11

2. Aerodynamic Performance of a Rotate-to-View Nose Missile;Journal of Spacecraft and Rockets;2001-03

3. Aerodynamic performance of a rotate to view nose missile - Trisonic flow, multibody interactions and optical fidelity studies;37th Aerospace Sciences Meeting and Exhibit;1999-01-11

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

5. Potential Flow Solutions with Wakes over an Ogive Cylinder;Journal of Spacecraft and Rockets;1998-05

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