The pitching-moment derivatives Cmq and Cma at supersonic speeds are developed for a slender-delta-wing and slender-body combination having no afterbody. By drawing an analogy between the aerodynamics of the wing-body section of the combination and the aerodynamics of a delta wing alone, the results for the slender-delta-wing and slender-body combination are modified to the extent that approximate solutions for Cmq and for broad-delta-wing and slender-body combinations can be obtained.


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    Titel :

    Pitching-Moment Derivatives Cmq and Cma at Supersonic Speeds for a Slender-Delta-Wing and Slender-Body Combination and Approximate Solutions for Broad-Delta-Wing and Slender-Body Combinations


    Beteiligte:
    A. Henderson (Autor:in)

    Erscheinungsdatum :

    1951


    Format / Umfang :

    33 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch