This paper has established the models calculating aero-optic effect of the hypersonic flying vehicle, and using a new turbulence hypothesis model, which is on base of Johnson- King & k-(epsilon) equation. Then the calculating program was designed. In the last part, the calculating result was discussed.


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    Title :

    Calculating aero-optic effect of turbulent flow on the hypersonic flying vehicle


    Contributors:

    Conference:

    Propagation and Imaging through the Atmosphere IV ; 2000 ; San Diego,CA,United States


    Published in:

    Proc. SPIE ; 4125 ; 102


    Publication date :

    2000-11-17





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English