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.


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    Titel :

    Aerodynamic characteristic of a swept-wing cruise missile at Mach numbers from 0.50 to 2.86


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

    Erscheinungsdatum :

    1972-11-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :