The problem of determining airplane aerodynamic model equations and estimating the associated parameters from flight data taken at high angles of attack is addressed. Two representations of the aerodynamic function based on the polynomial and spline representations are given. Then the technique of building an adequate model using a stepwise regression is presented with examples demonstrating the construction of the model and various approaches to model verification.


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    Title :

    Determination of airplane aerodynamic parameters from flight data at high angles of attack


    Contributors:

    Conference:

    International Council of the Aeronautical Sciences ; 1982 ; Seattle, WA


    Publication date :

    1982-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English