NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Structural modeling of aircraft tiresA theoretical and experimental investigation of the feasibility of determining the mechanical properties of aircraft tires from small-scale model tires was accomplished. The theoretical results indicate that the macroscopic static and dynamic mechanical properties of aircraft tires can be accurately determined from the scale model tires although the microscopic and thermal properties of aircraft tires can not. The experimental investigation was conducted on a scale model of a 40 x 12, 14 ply rated, type 7 aircraft tire with a scaling factor of 8.65. The experimental results indicate that the scale model tire exhibited the same static mechanical properties as the prototype tire when compared on a dimensionless basis. The structural modeling concept discussed in this report is believed to be exact for mechanical properties of aircraft tires under static, rolling, and transient conditions.
Document ID
19730012279
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Clark, S. K.
(Michigan Univ. Ann Arbor, MI, United States)
Dodge, R. N.
(Michigan Univ. Ann Arbor, MI, United States)
Lackey, J. I.
(Michigan Univ. Ann Arbor, MI, United States)
Nybakken, G. H.
(Michigan Univ. Ann Arbor, MI, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1973
Publication Information
Publisher: NASA
Subject Category
Aircraft
Report/Patent Number
REPT-05608-16-T-REV
NASA-CR-2220
Report Number: REPT-05608-16-T-REV
Report Number: NASA-CR-2220
Accession Number
73N21006
Funding Number(s)
PROJECT: RTOP 501-38-12-02
CONTRACT_GRANT: NGL-23-005-010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available