More general analysis and numerical example; analysis of nonequilibrium nozzle flow of ideal dissociating gas is generalized to encompass entire range of reference dissociation level in reaction-dominated regime; hypersonic restriction on analysis is also relaxed, although equilibrium-throat condition is still retained; results show that assessment of equilibrium-recombination and sudden-freezing models hold in general for reaction-dominated regime; numerical example is presented to compare results given by analysis and exact numerical solution; good agreement between them is obtained.


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    Title :

    Freezing of dissociation and recombination in supersonic nozzle flows -- 2


    Additional title:

    AIAA J


    Contributors:
    Lee, R.S. (author) / Cheng, H.K. (author)

    Published in:

    AIAA Journal ; 6 , n 5, Part 2


    Publication date :

    1968


    Size :

    15 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :