Prediction of projectile performance, stability and free-flight motion using CFD-Reference-Cited by-同舟云学术

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Prediction of projectile performance, stability and free-flight motion using CFD

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

Author:

Weinacht Paul¹,Weinacht Paul¹

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/10.2514/6.1997-421

Reference16 articles.

1. THE EFFECT OF LENGTH ON THE AERODYNAMIC CHARACTERISTICS OF BODIES OF REVOLUTION IN SUPERSONIC FLIGHT

2. Nietubicz, C.J., and Opalka, K. "Supersonic WindTunnel Measurements ofStaticand Magnus Aerodynamic Coefficients for Projectile Shapes with Tangent and Secant Ogive Noses," U.S. Army Ballistic Research Laboratory Memorandom Report ARBRL-MR-02991, Aberdeen Proving Ground, MD,February 1980.

3. Computational parametric study of the Magnus effect on boattailed shell at supersonic speeds

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1. Flight Mechanics of a Supersonic Projectile: A Parametric Investigation;AIAA SCITECH 2022 Forum;2022-01-03

2. Coning motion stability of wrap around fin rockets;Science in China Series E: Technological Sciences;2007-06

3. Experimental and Computational Assessment of the Dynamic Stability of a Supersonic Square Section Missile;22nd Applied Aerodynamics Conference and Exhibit;2004-06-20

4. Aerodynamic design of non-axisymmetric fuzes for guided munitions;23rd Atmospheric Flight Mechanics Conference;1998-08-10

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