Transient heat-transfer data obtained from thermal-capacitance rocket can be analyzed by number of methods; six techniques are discussed and applied to obtain local values of heat-transfer coefficients in ammonia-oxygen rocket; integration method appears to be best from standpoint of possible accuracy.
Application of various techniques for determining local heat-transfer coefficients in rocket engine from transient experimental data
NASA -- Tech Note
1960
33 pages
Report
English
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Determination of rocket-motor heat-transfer coefficients by transient method
Engineering Index Backfile | 1951
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