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Dynamic testing of airplane shock-absorbing strutsMeasurement of perpendicular impacts of a landing gear with different shock-absorbing struts against the drum testing stand. Tests were made with pneumatic shock absorbers having various degrees of damping, liquid shock absorbers, steel-spring shock absorbers and rigid struts. Falling tests and rolling tests. Maximum impact and gradual reduction of the impacts in number and time in the falling tests. Maximum impact and number of weaker impacts in rolling tests.
Document ID
19930094760
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Langer, P
Thome, W
Date Acquired
September 6, 2013
Publication Date
January 1, 1932
Report/Patent Number
NACA-TM-656
Report Number: NACA-TM-656
Accession Number
93R23680
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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