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Static Footprint Local Forces, Areas, and Aspect Ratios for Three Type 7 Aircraft TiresThe National Tire Modeling Program (NTMP) is a joint NASA/industry effort to improve the understanding of tire mechanics and develop accurate analytical design tools. This effort includes fundamental analytical and experimental research on the structural mechanics of tires. Footprint local forces, areas, and aspect ratios were measured. Local footprint forces in the vertical, lateral, and drag directions were measured with a special footprint force transducer. Measurements of the local forces in the footprint were obtained by positioning the transducer at specified locations within the footprint and externally loading the tires. Three tires were tested: (1) one representative of those used on the main landing gear of B-737 and DC-9 commercial transport airplanes, (2) a nose landing gear tire for the Space Shuttle Orbiter, and (3) a main landing gear tire for the Space Shuttle Orbiter. Data obtained for various inflation pressures and vertical loads are presented for two aircraft tires. The results are presented in graphical and tabulated forms.
Document ID
19910007701
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Howell, William E.
(NASA Langley Research Center Hampton, VA., United States)
Perez, Sharon E.
(NASA Langley Research Center Hampton, VA, United States)
Vogler, William A.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1991
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TP-2983
NAS 1.60:2983
L-16521
Report Number: NASA-TP-2983
Report Number: NAS 1.60:2983
Report Number: L-16521
Accession Number
91N17014
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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