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Frictional Power Intensity Measurements for Aircraft Tires WL/FIVMA, Wright Laboratory

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Medzorian, John P., author.
Conference Name:
Aerospace Atlantic Conference & Exposition (1995-05-23 : Dayton, Ohio, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1995
Summary:
This paper presents the results of tire footprint studies which were performed to understand the effects of vertical load, camber, yaw, inflation pressure and tire construction on frictional power. Two previously worn F-16 radial and bias tire constructions were selected. All tests were conducted at low speed on a Tire Force Machine having a specialized sensor plate with embedded traction and slip sensors. The tests indicate that the total frictional power for both tire constructions are quite similar at low yaw angles, however, at 4° yaw, the bias tire generated significantly more frictional power than the radial tire
Notes:
Vendor supplied data
Publisher Number:
951416
Access Restriction:
Restricted for use by site license

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