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Flight investigation of piloting techniques and crosswind limitations using a research type crosswind landing gearA research-type crosswind landing gear was tested in a flight program which used a light STOL transport in strong crosswind conditions. The research-type crosswind landing gear used enabled the airplane to land to crosswinds up to a magnitude of 25 to 30 knots. Three modes of landing-gear operation were investigated: preset, automatic, and castor (passive self-alignment). Actual test data and histograms are given for the 195 'visual flight rules' crosswind landings made.
Document ID
19790014841
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Fisher, B. D.
(NASA Langley Research Center Hampton, VA, United States)
Deal, P. L.
(NASA Langley Research Center Hampton, VA, United States)
Champine, R. A.
(NASA Langley Research Center Hampton, VA, United States)
Patton, J. M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-TP-1423
L-12682
Report Number: NASA-TP-1423
Report Number: L-12682
Accession Number
79N23012
Funding Number(s)
PROJECT: RTOP 505-08-33-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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