The Use of Rational Approximations in the Calculation of Flows with Detached Shocks-Reference-Cited by-同舟云学术

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The Use of Rational Approximations in the Calculation of Flows with Detached Shocks

Published:1960-07 Issue:7 Volume:27 Page:559-560
ISSN:1936-9999
Container-title:Journal of the Aerospace Sciences
language:en
Short-container-title:Journal of the Aerospace Sciences

Author:

Van Tuyl A. H.¹

Affiliation:

1. U. S. Naval Ordnance Laboratory, White Oak, Silver Spring, Md.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.8643

Reference10 articles.

1. Staff cf the Computing Section, (Under the direction of Zdenek Kopal), Tables of Supersonic Flow Around Cones, Center of Analysis, Dept. of Electrical Engineering, M.I.T., Tech. Report No. 1, 1947.

2. Ames Research Staff, Equations, Tables, and Charts for Compressible Flow, NACA Report 1135, 1953.

3. Hayes, W. D., and Probstein, R. F., Hypersonic Floiv Theory, p.143, Academic Press, New York, 1959.

Cited by 9 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. COMPUTER-EXTENDED SERIES;ANNU REV FLUID MECH;1984

2. The use of Pade fractions in the calculation of nozzle flows;Padé Approximants Method and Its Applications to Mechanics;1976

3. Series solution for the planar asymmetric blunt-body problem;Physics of Fluids;1975

4. Use of Pade fractions in the calculation of blunt body flows;AIAA Journal;1971-07

5. Initial Stages of Axisymmetric Shock-on-Shock Interaction for Blunt Bodies;Physics of Fluids;1970

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