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Material Response of One-Dimensional, Steady-State Transpiration Cooling in Radiative and Convective EnvironmentsA simplified analytical solution for thermal response of a transpiration-cooled porous heat-shield material in an intense radiative-convective heating environment is presented. Essential features of this approach are "two-flux method" for radiative transfer process and "two-temperature" assumption for solid and gas temperatures. Incident radiative-convective heatings are specified as boundary conditions. Sample results are shown using porous silica with CO2 transpiration and some parameters quantitatively show the effect on this transpiration cooling system. Summarized maps for mass injection rate, porosity and blowing correction factor for radiation are obtained in order to realize such a cooling system.
Document ID
19990069906
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
Kubota, Hirotoshi
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1975
Publication Information
Publisher: American Inst. of Aeronautics and Astronautics
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
T 75-17727
AIAA Paper 75-744
Meeting Information
Meeting: Thermophysics
Location: Denver, CO
Country: United States
Start Date: May 27, 1975
End Date: May 29, 1975
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other

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