Study made to investigate effect of slipstream span on lift increment due to thrust on wing with high lift flaps; comparison with results obtained on same model with two propellers showed that lift increment due to thrust was proportional to slipstream velocity and proportional to wing area in slipstream.


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    Title :

    Large-scale wind-tunnel tests of airplane model with unswept, aspect-ratio-10 wing, four propellers, and blowing flaps


    Additional title:

    NASA -- Tech Note


    Contributors:
    Weiberg, J.A. (author) / Page, V.R. (author)


    Publication date :

    1959


    Size :

    39 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :