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    Title :

    Effect of leading-edge geometry on boundary-layer transition at Mach 3.1


    Contributors:

    Publication date :

    1956-03-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



    Boundary-layer instability mechanisms on a swept-leading edge at Mach 3.5

    Creel, T.R. jun. / Malik, M.R. / Beckwith, I.E. | Tema Archive | 1987


    Boundary-Layer Instability Mechanisms on a Swept-Leading Edge at Mach 3.5

    Beckwith, I. E. / Malik, M. R. / Creel, T. R. | SAE Technical Papers | 1987



    Effect of Slight Leading Edge Bluntness on Flat Plate Heat Transfer and Boundary Layer Transition at Hypersonic Mach Numbers

    Hozumi, K. / Nagai, S. / Fujii, K. et al. | British Library Conference Proceedings | 1994


    Leading edge bluntness effects on laminar-turbulent boundary layer transition on a cooled flat plate at mach 7

    Heffner, K. / Arnal, D. / European Space Agency et al. | British Library Conference Proceedings | 1995