NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Effects of wing lift and weight on landing-gear loadsThe effects of wing lift and weight on maximum landing gear loads were investigated by drop testing a small landing gear with oleo shock strut in the Langley impact basin. Lift forces were mechanically applied to the dropping mass to produce wing lift factors between 1000 and 2500 pounds. The results show the relationship between lift force, weight, and landing-gear loads for a range of vertical velocities between 0 and 12 feet per second.
Document ID
19930083568
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lindquist, Dean C
Date Acquired
August 16, 2013
Publication Date
March 1, 1952
Report/Patent Number
NACA-TN-2645
Report Number: NACA-TN-2645
Accession Number
93R12858
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available