Note on shock reflection coefficient.-Reference-Cited by-同舟云学术

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Note on shock reflection coefficient.

Published:1967-02 Issue:2 Volume:5 Page:369-371
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

GERBER NATHAN¹

Affiliation:

1. Ballistic Research Laboratories, Aberdeen Proving Ground, Md.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.3984

Reference12 articles.

1. Maxwell, J. C., Scientific Papers (Dover Publications Inc., New York,1965), Vol.II, pp.175-177.

2. Analytical design for optimum filamentary pressure vessels

3. Noting Fig. 1, the shock reflection coefficient is defined as follows (as onp.232 of Ref. 6):

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Some geometric acoustic problems of one-dimensional unsteady and two-dimensional steady flows;Fluid Dynamics;1967-09

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