Linearized slender body theory is applied to computation of aerodynamic forces on oscillating, or deforming, body of revolution; time dependence is taken to be sinusoidal; apparent mass approximation is obtained for body of small radius; specific calculations are performed for body in rigid motion.


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    Titel :

    Unsteady aerodynamic forces on slender body of revolution in supersonic flow


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Bond, R. (Autor:in) / Packard, B.B. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    32 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Unsteady aerodynamic forces on slender supersonic aircraft with flexible wings and bodies

    Yates, J.E. / Zeydel, E.F.E. | Engineering Index Backfile | 1963


    Flow over slender body of revolution at supersonic velocities

    Jones, R.T. / Margolis, B. | Engineering Index Backfile | 1946


    Flow over a slender body of revolution at supersonic velocities

    Jones, Robert T. / Margolies, Kenneth | TIBKAT | 1946