Reverse-flow relations provide convenient expressions for aerodynamic forces which act on general wing-fuselage combination; drag, lift, spanwise and chordwise lift distributions, and wing moments are treated; available methods and results are considered which apply to wing-fuselage interference problem; reverse-flow relations are then employed to effect desirable changes in defining force expressions by introducing wings or fuselages in reverse flow.


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    Title :

    Forces on wing-fuselage combinations in supersonic flow


    Additional title:

    J Fluid Mechanics


    Contributors:

    Published in:

    Publication date :

    1960


    Size :

    17 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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