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  • 1
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    On Landing Gear Stresses (1956)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: Information on landing gear stresses is presented on the following: vibratory phenomena, tangential forces applied to landing gear, fore and aft oscillations of landing gears, examples of fatigue failures, vibration calculations, and improvement of existing test equipment.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-TM-1422 , Sur les Sollicitations des Atterrisseurs; 25; 17-38
    Format: application/pdf
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