Aerodynamic interference for supersonic low-aspect-ratio missiles-Reference-Cited by-同舟云学术

Aerodynamic interference for supersonic low-aspect-ratio missiles

Published:1995-03 Issue:2 Volume:32 Page:270-278
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Nelson H. F.¹,Bossi Brent W.¹

Affiliation:

1. University of Missouri—Rolla, Rolla, Missouri 65401

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.26606

Reference38 articles.

1. ^ielsen, J. N. Hemsch,M. J., and Smith, C. A. "A Preliminary Method for Calculating the Aerodynamic Characteristics of Cruciform Missiles to High Angles of Attack Including Effects of Roll Angle and ControlDeflections," Office of Naval Research, Report ONR-CR215-226-4F, Nov. 1977.

2. Predicting the supersonic aerodynamics of very-low-aspect-ratio lifting surfaces

3. Supersonic Wing-Body Lift

4. 5Bruns, K. D., Moore, M. E., Stoy, S. L., Vukelich, S. R., and Blake, W. B. "MISSILE DATCOM-Revision 4/91," Wright-Patterson Air Force Base, Report WL-TR-91-3039, April 1991.

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1. An Engineering Method for Very Low Aspect Ratio Cruciform Wing-Body Configurations;31st AIAA Applied Aerodynamics Conference;2013-06-22

2. Aerodynamic Interference for Hypersonic Missiles at Low Angle of Attack;Journal of Spacecraft and Rockets;1998-11

3. Aerodynamic interference for hypersonic missiles at low angle of attack;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12