A Productivity-Oriented Application of Computational Fluid Dynamics to the Design of a Hypervelocity Missile-Reference-Cited by-同舟云学术

A Productivity-Oriented Application of Computational Fluid Dynamics to the Design of a Hypervelocity Missile

Published:2002-06-24 Issue: Volume: Page:
ISSN:
Container-title:20th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Vaughn Milton¹,Auman Lamar¹

Affiliation:

1. U.S. Army Aviation and Missile Command

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-2937

Reference18 articles.

1. Missile DATCOM. Volume 1

2. Moore, F. G., Mcinville, R. M., and Hymer, T. "The 1998 Version of the NSWCDD Aeroprediction Code: Part II - Program User's Guide and Source Code Listing," NSWCDD/TR98/73, May1998.

3. Lesieutre, D. J., Love, J. F., and Dillenius, M. F. E. "MISL3 - November 2000 Aerodynamic Analysis for Finned Vehicles with Axisymmetric Bodies," NEARTR561, May2001.

4. Gentry, A. E., Smyth, D. N., and Oliver, W. R. "The Mark IV Supersonic-Hypersonic Arbitrary Body Program, VolumeI Users Manual," Technical Report AFFDL-TR-73-159, November 1973.

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