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Influence of Wing Flexibility on Force-time Relation in Shock Strut Following Vertical Landing Impact
Document ID
19930082710
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mcpherson, Albert E (National Bureau of Standards)
Evans, J (National Bureau of Standards)
Levy, Samuel (National Bureau of Standards)
Date Acquired
August 16, 2013
Publication Date
November 1, 1949
Report/Patent Number
NACA-TN-1995
Report Number: NACA-TN-1995
Accession Number
93R12000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK ABSORBERS - STRUTS
LOADS, LANDING
WINGS, FLEXIBLE
LOADS - LANDING GEARS
LANDING GEARS - IMPACT

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