Purpose of paper is to consolidate available theoretical and experimental data for applicable drag and heat-transfer coefficients to provide empirical relationships useful for wide range of rocket nozzle conditions; some results presented show effect of these corrections on typical calculations of particle velocities and temperatures in rocket nozzles; inertial and compressibility effects dominate for large particles and high chamber pressures, causing thermal and velocity lags to be less than those predicted under Stokes flow assumption.


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    Title :

    Particle drag and heat transfer in rocket nozzles


    Additional title:

    AIAA J


    Contributors:

    Published in:

    AIAA Journal ; 2 , n 11


    Publication date :

    1964


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Particle drag and heat transfer in rocket nozzles

    CARLSON, D. J. / HOGLUND, R. F. | AIAA | 1964


    Analysis of heat transfer in rocket nozzles

    Keizers, H. / Veraar, R. | AIAA | 1996


    Analysis of Heat Transfer in Rocket Nozzles

    Keizers, H. L. J. / Veraar, R. G. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1996