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.
Determination of airplane aerodynamic parameters from flight data at high angles of attack
International Council of the Aeronautical Sciences ; 1982 ; Seattle, WA
01.01.1982
Sonstige
Keine Angabe
Englisch
Unsteady aerodynamic modeling and identification of airplane at high angles of attack
British Library Online Contents | 1996
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