Geometric variables covered included horizontal-tail chord, horizontal tail-span, vertical location of horizontal tail, and horizontal-tail dihedral angle; calculations were restricted to configurations having vertical tail of aspect ratio 1.0.


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    Title :

    Effect of horizontal-tail chord on calculated subsonic span loads and stability derivatives of isolated unswept tail assemblies in sideslip and steady roll


    Additional title:

    NASA -- Memo


    Contributors:
    Booth, K.W. (author)


    Publication date :

    1959


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :