A Six-Part Survey: Rocket Heat-Transfer Literature

[+] Author and Article Information
Thomas F. Irvine

North Carolina State College

R. W. Graham, G. Morrell, R. G. Deissler

Lewis Research Center, NASA, Cleveland, Ohio

R. D. Turnacliff

Space Technology Laboratory, Los Angeles, California

J. H. Robinson, K. G. Englar

Douglas Aircraft Company, Inc., El Segundo, Calif.

D. R. Bartz

Jet Propulsion Laboratory, Pasadena, Calif.

H. N. McManus

Cornell University, Ithaca, N. Y.

Erich E. Soehngen

Aeronautical Research Laboratory, WADC, Dayton, Ohio

J. Heat Transfer 82(3), 155-169 (Aug 01, 1960) (15 pages) doi:10.1115/1.3679899 History:


The survey has been divided into the following parts: Rocket-Engine Heat Sources; Rocket Cooling Techniques; Nozzle Wall Materials; Variable Fluid-Property Effects; Predictions of Thermal Properties; Flow Separation and Acoustic Effects.

Copyright © 1960 by ASME
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