A method has been developed for computing aerodynamic loads on slender missiles with complicated cross-sections. This method has been applied to the prediction of loads for missiles with folding wings. Comparison of theoretical calculations with supersonic wind-tunnel measurements indicates that the method should provide satisfactory first estimates of the aerodynamic properties of missiles with folding wings. A series of design charts is presented to allow rapid estimation of lift, folding moment and span loading for a wide variety of folding-wing configurations.


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    Titel :

    Characteristics of Slender Wing-Body Combinations with Folding Wings


    Untertitel :

    A Method of Computing Aerodynamic Loads on Slender Bodies of Complicated Cross-section


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.01.1959


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch