Test covered transition speed range from hovering to normal flight with flaps retracted; variables in testing were flap deflection, thrust coefficient, stabilizer incidence, ground proximity, and blowing boundary layer control effectiveness.


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    Title :

    Investigation of longitudinal and lateral stability characteristics of six-propeller deflected-slipstream VTOL model with boundary-layer control including effects of ground proximity


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    98 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :