0
RESEARCH PAPERS

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

Abstract

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
Your Session has timed out. Please sign back in to continue.

References

Figures

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In