A method is given for determining the horizontal tail loads in maneuvering flight. The method is based upon the assignment of a load-factor variation with time and the determination of a minimum time to reach peak load factor. The tail load is separated into various components. Examination of these components indicated that one of the components was so small that it could be neglected for most conventional airplanes, thereby reducing to a minimum number of aerodynamic parameters needed in this computation of tail loads.


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    Titel :

    Horizontal Tail Loads in Maneuvering Flight


    Beteiligte:
    H. A. Pearson (Autor:in) / W. A. McGowan (Autor:in) / J. J. Donegan (Autor:in)

    Erscheinungsdatum :

    1950


    Format / Umfang :

    33 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Horizontal tail loads in maneuvering flight

    Pearson, Henry A. / McGowan, William A. / Donegan, James J. | TIBKAT | 1950


    Horizontal tail loads in maneuvering flight

    Pearson, Henry A / Mcgowna, William A / Donegan, James J | NTRS | 1950


    Horizontal tail loads in maneuvering flight

    Pearson, Henry A / Mcgowan, William A / Donegan, James J | NTRS | 1951


    Horizontal tail loads in maneuvering flight

    Pearson, H.A. / McGowan, W.A. / Donegan, J.J. | Engineering Index Backfile | 1950


    Horizontal Tail Loads

    Lomax, Ted L. | AIAA | 1996