Hypersonic Viscous Flow Over Slender Cones-Reference-Cited by-同舟云学术

Hypersonic Viscous Flow Over Slender Cones

Published:1959-11 Issue:11 Volume:26 Page:723-730
ISSN:1936-9999
Container-title:Journal of the Aerospace Sciences
language:en
Short-container-title:Journal of the Aerospace Sciences

Author:

TALBOT L.¹,KOGA T.¹,SHERMAN P. M.¹

Affiliation:

1. University of California at Berkeley, and University of Michigan,

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.8282

Reference32 articles.

1. Maslach, G. J., and Sherman, F. S., Design and Testing o^ an Axisymmetric Hypersonic Nozzle for a Low Density Wind Tunnel, University of California Engineering Project Report HE-150-134, Series23, Issue 17,February, 1956.

2. Van Dyke, M. D., Practical Calculation of Second Order-Supersonic Flow Past Nonlifting Bodies of Revolution, NACA T N 2744,1952.

3. Kopal, Z., Tables of Supersonic Flow of Air Around Cones, Tech. Report No. 1, Massachusetts Institute of Technology, Cambridge, 1947.

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