Method developed to estimate magnitude of these loads in wing for two-wheel landing condition; wing is found to vibrate in such manner that points of attachment of landing gear are always two of node points.


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    Titel :

    Dynamic loads in airplane structures during landing


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Shou-Ngo Tu (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1946


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Dynamic loads on airplane structures during landing

    Biot, M. A. / Bisplinghoff, R. L. | TIBKAT | 1944


    Analytical and experimental studies on dynamic loads in airplane structures during landing

    Pian, T.H.H. / Flomenhoft, H.I. | Engineering Index Backfile | 1951


    DYNAMIC LOADS ON AIRPLANE STRUCTURES

    PANCU, C. D. P. / JENKINS, E. S. | SAE Technical Papers | 1949


    On actual loads on airplane landing gears

    Shiskin, S. | Engineering Index Backfile | 1937