Present high performance rocket engine presents many new heat transfer problems which are beyond range of previous work and not adequately covered by existing theory; some basic problems discussed and possible reasons for inability of conventional formulas and theories to correlate actual rocket motor heat transfer data given; several techniques for handling high heat flux rates and their applicability are mentioned.
Heat-transfer problems in liquid-propellant rocket motors
Am Rocket Soc -- J
1950
14 pages
Article (Journal)
English
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