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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    Titel :

    Calculation of aerodynamic characteristics of STOL aircraft


    Beteiligte:

    Erscheinungsdatum :

    01.11.1974


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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