
Accession Number : ADA193616
Title : A Critical Speed Study for Aircraft Bias Ply Tires.
Descriptive Note : Final rept. Oct 86Aug 87,
Corporate Author : AIR FORCE WRIGHT AERONAUTICAL LABS WRIGHTPATTERSON AFB OH
Personal Author(s) : Champion, John H ; Wagner, Paul M
PDF Url : ADA193616
Report Date : Jan 1988
Pagination or Media Count : 60
Abstract : This report describes the derivation and validation of the critical speed equation that predicts the inceptive speed of the standing wave in the tread band of aircraft bias tires. The critical speed equation is based on the classical theory of a straight beam on an elastic foundation, under tension. Derivations of relations describing each term of the critical speed equation are also presented. These relations describe the effective tire structural properties such as the tread band bending stiffness, the elastic foundation linear spring constant, the belt tension due to inflation pressure, and the tread band effective density. Dynamometer tests of a 49x17/26PR Type VII Goodyear tire was conducted to validate the critical speed equation. Trends relating critical speed with inflation pressure, tread depth, and loaded vertical deflection were correctly predicted, yielding an average of 2.9percent error. Keywords: Critical speed, Tire dynamics, Aircraft tire, Standing wave, Tire structural properties, Traction wave.
Descriptors : *AIRCRAFT TIRES, *ELASTIC PROPERTIES, DYNAMICS, DYNAMOMETERS, EQUATIONS, STANDING WAVES, STRUCTURAL PROPERTIES, TENSION, TEST METHODS, TRACTION, TREADS, VELOCITY, RUBBER, MATHEMATICAL ANALYSIS, PERFORMANCE(ENGINEERING)
Subject Categories : Aircraft
Elastomers and Rubber
Distribution Statement : APPROVED FOR PUBLIC RELEASE