Experimental procedure developed to measure gas film heat transfer coefficients in rocket motor combustion chambers and nozzles; procedure utilizes transient temperature rise of uncooled segmented walls of rocket motor to determine rate of heat transfer.
Determination of rocket-motor heat-transfer coefficients by transient method
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 18 , n 8
1951
Article (Journal)
English
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