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Theoretical dynamic analysis of the landing loads on a vehicle with a tricycle landing gearTheoretical dynamic analysis of landing loads on vehicle with tricycle landing gear compared with X-15 aircraft data
Document ID
19670023065
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Mc Kay, J. M. (NASA Flight Research Center Edwards, CA, United States)
Noll, R. B. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-4075
Report Number: NASA-TN-D-4075
Accession Number
67N32394
Funding Number(s)
CONTRACT_GRANT: 719-01-00-04-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LANDING GEAR
DYNAMIC LOAD
STRESS ANALYSIS
X-15 AIRCRAFT

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