In this paper, the integration of wind tunnel and flight test procedures are studied for specifying aerodynamic model forms. A procedure is described which employs a stepwise regression method to systematically determine model structures and F-ratio statistics to rank the importance of each aerodynamic coefficient within a given model. Application of this technique and wind tunnel procedures to an oblique-wing aircraft indicate that the aircraft's measured and estimated response are in good agreement at both small and large wing skew angles


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    Title :

    Determination of an oblique wing aircraft's aerodynamic characteristics


    Contributors:
    Travassos, R. H. (author) / Gupta, N. K. (author) / Iliff, K. W. (author) / Maine, R. (author)

    Conference:

    Atmospheric Flight Mechanics Conference ; 1980 ; Danvers, MA


    Publication date :

    1980-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :