To study shock layer radiative phenomena, experimental studies of equilibrium radiative heating during re-entry were undertaken at Ohio State University; using arc-driven shock-tube facility, measurements of total stagnation-point equilibrium radiative heat flux in wavelength region of 0.17 to 6.0 Μ were carried out over range of simulated flight velocities from 26,000 to 52,000 fps and at simulated altitudes from 100,000 to 170,000 ft; experimental techniques applied, and results obtained are reported.


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    Title :

    Shock-tube studies of equilibrium air radiation


    Additional title:

    AIAA J


    Contributors:

    Published in:

    AIAA Journal ; 3 , n 6


    Publication date :

    1965


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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