An investigation was made to determine the aerodynamic characteristics of an airbreathing missile configuration having a forward located inlet. Control was provided by cruciform tail surfaces. Aerodynamic data were obtained for the body-tail configuration alone and with planar or cruciform wings. At Mach numbers from 2.86 to 4.63, the model had internal flow. At Mach numbers from 1.70 to 2.86, the internal duct was closed, and an inlet fairing was installed to simulate boost conditions.


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    Titel :

    Stability and control characteristics of an air-breathing missile configuration having a forward located inlet


    Beteiligte:
    Sawyer, W. C. (Autor:in) / Hayes, C. (Autor:in)

    Erscheinungsdatum :

    1976-07-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Hypersonic Air-Breathing Missile Propulsion

    Waltrup, P. J. / Advisory Group for Aerospace Research and Development | British Library Conference Proceedings | 1997



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