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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    Titel :

    Shock-tube studies of equilibrium air radiation


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Nerem, R.M. (Autor:in) / Stickford, G.H. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 6


    Erscheinungsdatum :

    1965


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Shock-tube studies of equilibrium air radiation

    NEREM, R. M. / STICKFORD, G. H. | AIAA | 1965


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    Shock Tube Experimental Studies on

    Xiong, X. H | Online Contents | 2017


    Radiation calculation in non-equilibrium shock layer

    Dubois, J. / European Space Agency | British Library Conference Proceedings | 2005