Effect of space limitations on spring performance is analyzed and leads to optimum design formulas for three most common types of aircraft springs, i.e., tension, compression, and torsion springs; using formulas thus derived, for given allowable stress relationship between space limitations, maximum load obtainable and corresponding wire size can be found immediately.


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    Titel :

    Space limitations and optimum conditions in aircraft spring design


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Carter, R.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1943


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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