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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Unsteady aerodynamic forces on slender body of revolution in supersonic flow


    Additional title:

    NASA -- Tech Note


    Contributors:
    Bond, R. (author) / Packard, B.B. (author)


    Publication date :

    1961


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



    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