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:
    Morote, J. (author) / Liaño, G. (author) / Jiménez, J. (author)

    Published in:

    Publication date :

    2017-01-31


    Size :

    12 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Nonlinear Rolling Motion of Triform Finned Missiles

    Morote, Jesus / Liaño, Gabriel / Jiménez, José | AIAA | 2016




    Analysis of the nonlinear rolling motion of finned missiles

    COHEN, C. / CLARE, T. / STEVENS, F. | AIAA | 1972


    Analysis of the Nonlinear Rolling Motion of Finned Missiles

    CHARLES J. CONEN / THOMAS A. CLARE / AND FRANK L. STEVENS | AIAA | 1974