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.


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    Title :

    Application of various techniques for determining local heat-transfer coefficients in rocket engine from transient experimental data


    Additional title:

    NASA -- Tech Note


    Contributors:
    Liebert, C.H. (author) / Hatch, J.E. (author) / Grant, R.W. (author)


    Publication date :

    1960


    Size :

    33 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :