Experimental heat-transfer study of shock impingement on fins in hypersonic flow-Reference-Cited by-同舟云学术

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Experimental heat-transfer study of shock impingement on fins in hypersonic flow

Published:1965-07 Issue:4 Volume:2 Page:630-632
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

FRANCIS W. LEON¹

Affiliation:

1. Ford Motor Company, Newport Beach, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.28253

Reference6 articles.

1. Ferri, A., Elements of Aerodynamics of Supersonic Flows (The Macmillan Co., New York, 1949), Chap. 4, pp.73-74.

2. Hoshizaki, H. "Mass transfer and shock generated vorticity/' AHS J. 30, 628-634 (1960).

3. Theory of Stagnation Point Heat Transfer in Dissociated Air

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1. Flow Structure and Heat Transfer Characterization of a Blunt-Fin-Induced Shock-Wave/Laminar Boundary-Layer Interaction;AIAA Scitech 2021 Forum;2021-01-04

2. Shock interactions in hypersonic flows outside the sonic circle in front of a blunt body;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-04-30

3. Analytical Solution of the Type IV Shock Interaction;Journal of Propulsion and Power;1997-09

4. Analytical solutions of hypersonic type IV shock-shock interactions on noncircular bodies;Space Plane and Hypersonic Systems and Technology Conference;1996-11-18

5. Computational analysis of the unsteady type IV shock interaction of blunt body flows;Journal of Propulsion and Power;1996-01

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