The aerodynamic forces acting on a missile in consequence of small perturbations from a prescribed trajectory are calculated on the basis of slender body theory and piston theory is applied, in some detail, to the specific example of Generalized Missile Dynamics Analysis, II Equations of Motion.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Generalized Missile Dynamics Analysis. III. Aerodynamics


    Contributors:
    J. W. Miles (author) / D. Young (author)

    Publication date :

    1958


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Missile aerodynamics

    Nielsen, Jack N. | SLUB | 1988



    Missile Aerodynamics: NEAR Conference on Missile Aerodynamics

    M. R. Mendenhall / D. Nixon / M. F. E. Dillenius | NTIS | 1988