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Landing-gear impactReport deals with the impact forces in landing gears. Both the landing impact and the taxiing impact have been considered, but drag forces have so far been excluded. The differential equations are developed and their numerical integration is shown, considering the nonlinear properties of the oleo shock strut. A way is shown for determining the dimensions of the metering pin from a given load-time diagram. A review of German literature on landing-gear impact is also presented.
Document ID
19930083479
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Flugge, W (Stanford University)
Date Acquired
August 16, 2013
Publication Date
October 1, 1952
Report/Patent Number
NACA-TN-2743
Accession Number
93R12769
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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