Viscous CFD calculations of grid fin missile aerodynamics in the supersonic flow regime-Reference-Cited by-同舟云学术

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Viscous CFD calculations of grid fin missile aerodynamics in the supersonic flow regime

Published:2001-01-08 Issue: Volume: Page:
ISSN:
Container-title:39th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

DeSpirito James¹,Sahu Jubaraj¹

Affiliation:

1. U.S. Army, Research Lab., Aberdeen Proving Ground, MD

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-257

Reference27 articles.

1. Washington, W. D., and Miller, M. S. "Grid Fins-A New Concept for Missile Stability and Control,"AIAA Paper 93-0035, January 1993.

2. An experimental investigation of grid fin drag reduction techniques

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