The objective of the work described in this report was to develop a better understanding of the aerodynamic roll characteristics of canard controlled missiles. Studies were performed to develop a method of predicting induced roll moments, a method for simplified representation of aerodynamic coefficients in simulations, and to evaluate the use of canard and tail slots.


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    Title :

    Advanced Aerodynamic Control Technology


    Contributors:

    Publication date :

    1975


    Size :

    37 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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