Estimation of the aerodynamic normal force and static moment of a given class of flight vehicles is demonstrated with reference to AMCP 706-280, which in turn derives from the classic British work 'Wings'. By means of linearized algebraic reduction, a transmutation permits the designer to quickly evaluate the effects of variation on the flight system.


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    Title :

    Algorithm for Estimating Aerodynamic Static Moments of Long Rod Penetrators at 2 Less than M Less than 5


    Contributors:

    Publication date :

    1980


    Size :

    49 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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