Convective and radiative heat transfer to an ablating body.-Reference-Cited by-同舟云学术

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Convective and radiative heat transfer to an ablating body.

Published:1968-08 Issue:8 Volume:6 Page:1441-1449
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

HOSHIZAKI H.¹,LASHER L. E.¹

Affiliation:

1. Lockheed Polo Alto Research Laboratory, Polo Alto, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.4786

Reference22 articles.

1. Howe, J. T. and Sheaffer, Y. S. "Mass Addition in the Stagnation Region For Velocities Up to 50,000 Feet Per Second," TR R-207, Aug.1964, NASA.

2. Convective and radiative heat transfer during superorbital entry

3. Hayes, W. D. and Probstein, R. F., Hypersonic Flow Theory, Academic, New York, 1959, pp.388-389.

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