Most of the aerodynamic configurations considered are suitable for highly maneuverable air-to-air or surface-to-air missiles; however, data for a few air-to-surface, cruise missiles, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range.


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    Title :

    Analysis and compilation of missile aerodynamic data. Volume 1: Data presentation and analysis


    Contributors:

    Publication date :

    1977-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :