Near wake of a hypersonic blunt body with mass addition-Reference-Cited by-同舟云学术

Near wake of a hypersonic blunt body with mass addition

Published:1970-05 Issue:5 Volume:8 Page:833-842
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

COLLINS DONALD J.¹,LEES LESTER¹,ROSHKO ANATOL¹

Affiliation:

1. California Institute of Technology, Pasadena, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.5775

Reference21 articles.

1. Presented as Paper 69-67 at the AIAA 7th Aerospace Sciences Meeting, New York, January20-22,1969; submitted December 23, 1968; revision received July 28, 1969. The work discussed in this paper was carried out under the sponsorship and with the financial support of the U.S. Army Research Office and the Advanced Research Projects Agency, Contract DA-31-124-ARO(D)-33. This research is a part of Project DEFENDER sponsored by the Advanced Research Projects Agency.

2. Collins, D. J. "The Near Wake of a Two-Dimensional Hypersonic Blunt Body with Mass Addition," Ph.D. thesis,Dec. 1968,CaliforniaInstitute of Technology, Pasadena, Calif.

3. Theory of laminar near wake of blunt bodies in hypersonic flow.

4. Klineberg, J. M. "Theory of Laminar Viscous-Inviscid Interactions in Supersonic Flow," Ph.D. thesis,June 1968, California Institute of Technology, Pasadena, Calif.

5. A study of wakes behind a circular cylinder at m equal 5.7

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