Abstract The dynamic wind-tunnel tests of a functional model of a flight vehicle being developed make it possible to obtain more reliable data on aerodynamic and structural characteristics and, hence, improve the design quality and increase reliability in the finished product operation. The objective stated is achieved by formation of angular model motions, the parameters of which are measured and compared with angular parameters calculated using the analytical solutions of differential equations of motions being formed. We considered two media of the incoming flow with the resistance proportional to speed and the square of speed. The results can be used in flight vehicle design, development of onboard control algorithms and subsequent identification of other parameters.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Analytical parametric identification in dynamic wind-tunnel tests


    Contributors:

    Published in:

    Publication date :

    2007-03-01


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    Two-point Aerodynamic Model Identification from Dynamic Wind Tunnel Tests

    Dias, Joaquim N. / Girardi, Roberto D. | AIAA | 2016


    Wind tunnel tests

    Online Contents | 1993


    Parameter identification by free-flight wind tunnel tests

    Nowack, J. / Alles, W. | Tema Archive | 2008


    Free Flight Wind Tunnel Tests for Parameter Identification

    Nowack, J. / Alles, W. | British Library Conference Proceedings | 2008