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)


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    Titel :

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


    Beteiligte:
    M. L. Spearman (Autor:in) / I. K. Collins (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    44 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch