An investigation has been made in the Mach number range from 0.50 to 2.86 to determine the longitudinal and lateral aerodynamic characteristics of a cruise missile having a 58 deg swept wing and conventional aft tails. Such a vehicle might be applicable to missions such as surface- or air-launched tactical or strategic missiles, unmanned reconnaissance, or countermeasure decoys. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic Characteristic of a Swept-Wing Cruise Missile at Mach Numbers from 0.50 to 2.86


    Contributors:

    Publication date :

    1972


    Size :

    44 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English