Lateral oscillations of sting-mounted models at high alpha-Reference-Cited by-同舟云学术

Lateral oscillations of sting-mounted models at high alpha

Published:1990-09 Issue:5 Volume:27 Page:508-513
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Ericsson L. E.¹

Affiliation:

1. Lockheed Missiles & Space Company, Inc., Sunnyvale, California 94089

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.26173

Reference20 articles.

1. 3Keener, E. R., Chapman, G. T., and Kruse, R. L. "Effects of Mach Number and Afterbody Length on Onset of Asymmetric Forces on Bodies at Zero Sideslip and High Angles of Attack," AIAA Paper 76-0066, Jan. 1976.

2. Reynolds number effect on the aerodynamic characteristics of an ogive-cylinder at high angles of attack

3. 5Lamorit, P. J. "The Complex Asymmetric Flow Over a 3-5 D Ogive Nose and Cylindrical Afterbody at High Angles of Attack," AIAA Paper 82-0053, Jan. l£82.

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