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    Title :

    Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07


    Contributors:

    Publication date :

    1958-03-24


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Transition on swept leading edges at Mach 3.5

    Creel, T. R., Jr. / Beckwith, I. E. / Chen, F. J. | NTRS | 1987


    Transition on swept leading edges at Mach 3.5

    CREEL, T. R. / BECKWITH, I. E. / CHEN, F. J. | AIAA | 1987


    Leading edge transition on a 76 degree swept cylinder at Mach 1.6

    Coleman, Colin / Laub, James / Poll, D. et al. | AIAA | 1996