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Technique for measuring side forces on a banked aircraft with a free-swiveling nose gearAn experimental investigation was conducted at the Langley Research Center to determine a method for towing an aircraft to measure the side forces of a free-swiveling nose gear due to variations in bank angle. A F-106 aircraft and the Space Shuttle orbiter OV-101 were towed to measure side forces on full-size aircraft for bank angles up to 3 deg. These tests indicate that substantial side forces will occur if an aircraft is rolling on a runway in a banked attitude even when the nose gear is free to swivel. Corotation of a twin-tire nose gear appears to cause a substantial increase in side force due to bank angle compared with a nose gear with indepdendently rotating wheels.
Document ID
19860020761
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stubbs, S. M.
(NASA Langley Research Center Hampton, VA, United States)
Tanner, J. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1986
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:87719
L-16137
NASA-TM-87719
Report Number: NAS 1.15:87719
Report Number: L-16137
Report Number: NASA-TM-87719
Accession Number
86N30233
Funding Number(s)
PROJECT: RTOP 505-63-41-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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