A theoretical investigation of the rolling motion of triform configurations at high angles of attack is presented. A nonlinear aerodynamic flow model, derived from strip and slender body theories, is used to predict the aerodynamic roll coefficients of triform tailed missiles at high angles of attack. The flow model predictions are compared to the estimates of a panel-based code and a computational fluid dynamics code at two Mach numbers.


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    Title :

    Nonlinear Rolling Motion of Triform Finned Missiles


    Contributors:


    Publication date :

    2017




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    Local classification TIB:    770/7040
    BKL:    55.60 Raumfahrttechnik




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    Nonlinear Rolling Motion of Triform Finned Missiles

    Morote, J. / Liaño, G. / Jiménez, J. | AIAA | 2017


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