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On Landing Gear StressesInformation 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.
Document ID
20030065915
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Gentric, A. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 21, 2013
Publication Date
July 1, 1956
Publication Information
Publication: Sur les Sollicitations des Atterrisseurs
Issue: 25
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-TM-1422
Report Number: NACA-TM-1422
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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