Power-off tests conducted to determine dynamic stability of model with 42° swept back wing of aspect ratio 5.9 and taper ratio 0.45; results showed that, although wing alone was statically unstable longitudinally at moderate and high lift coefficients, complete model was practically stable over lift range for some horizontal tail positions.


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    Title :

    Flight tests of airplane model with 42° swept-back wing in Langley free-plight tunnel


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Maggin, B. (author) / Bennett, C.V. (author)


    Publication date :

    1947


    Size :

    14 pages


    Remarks:

    14 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :