Method predicts lift and pitching moment characteristics of STOL aircraft with externally-blown, jet-augmented wing-flap combinations using potential-flow approach which involves combination of two flow models. Method can accommodate multiple engines per wing panel and part-span flaps.


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    Title :

    Calculation of aerodynamic characteristics of STOL aircraft


    Contributors:

    Publication date :

    1974-11-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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