Aerodynamics of hypersonic flight at altitudes wherein laws of continuum flow theory apply; expressions for lift, drag, and pitching moment coefficients derived; application to various airfoil sections; airfoil formulas can be applied to finite wings with reasonable accuracy for design estimations.


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    Title :

    Two-dimensional airfoils at moderate hypersonic velocities


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1952


    Size :

    8 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Two-dimensional airfoils in hypersonic flows

    Linnell, R.D. | Engineering Index Backfile | 1949




    Oblique Detonation at Hypersonic Velocities

    Leyer, J.-C. / Borisov, A. A. / Kuhl, A. L. et al. | AIAA | 1991


    Heatshield materials erosion at hypersonic velocities

    MCMILLEN, L. / DUNBAR, L. / JACKSON, D. | AIAA | 1976