An investigation has been conducted in the Langley stability tunnel to determine the effect of an unswept wing on the contribution of unswept-tail configurations to the low-speed static and rolling-stability derivatives of a midwing airplane model.


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    Title :

    Effect of an Unswept Wing on the Contribution of Unswept-Tail Configurations to the Low-Speed Static- and Rolling-Stability Derivatives of a Midwing Airplane Model


    Contributors:
    W. Letko (author) / D. R. Riley (author)

    Publication date :

    1950


    Size :

    46 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English