An investigation of flow separation and aerodynamic controls at hypersonic speeds.-Reference-Cited by-同舟云学术

An investigation of flow separation and aerodynamic controls at hypersonic speeds.

Published:1966-11 Issue:6 Volume:3 Page:555-561
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

KAUFMAN L. G.¹,MECKLER L.¹,HARTOFILIS S. A.¹

Affiliation:

1. Grumman Aircraft Engineering Corporation, Bethpage, N. Y.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.43776

Reference7 articles.

1. Kaufman, L. (J., II, Oman, "II. A., Ilartoniis, S. A., Meckler, L. I I . , Kvans, W. J., and Weiss, 1). "'A review of hypersonic,' flow separation and control characteristics/' Aeronautical Systems Division, AS D-T 1)11-62-16S (March 1962). '2Kaufman, L. (}., II, Meckler, L. I I . , Ihirtofilis, S. A., and Weiss, I). "An investigation of hypersonic flow separation and control characteristics, Air Force Flight Dynamics Lab., AFFDL-Tll 64-174 (January 1965).

2. June 1965;Meckler L. I I .

3. Mach 8 to 22 studies of flow separations due to deflected control surfaces

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