Thermal Response of a Transpiration-Cooled System in a Radiative and Convective Environment

[+] Author and Article Information
H. Kubota

National Aerospace Laboratory, Chofu, Tokyo, Japan

J. Heat Transfer 99(4), 628-633 (Nov 01, 1977) (6 pages) doi:10.1115/1.3450753 History: Received November 29, 1976; Online August 11, 2010


The unsteady thermal response of a one-dimensional transpiration-cooled system in a radiative and convective environment is presented. The governing equations are solved by the Hartree-Womersley differential-difference method. The solid and fluid temperatures, the fluid pressure distributions, and the back-face heat transfer rate are obtained for a sample case of a 15 degree-entry into a Saturn nominal atmosphere.

Copyright © 1977 by ASME
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