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Wear, friction, and temperature characteristics of an aircraft tire undergoing braking and cornering

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:46:49Z
date available2017-09-04T17:46:49Z
date copyright01/01/1979
date issued1979
identifier otherENBBFEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/170034
description abstractAn investigation to evaluate the wear, friction, and temperature characteristics of aircraft tire treads fabricated from different elastomers is presented. The braking and cornering tests performed on aircraft tires retreaded with currently employed and experimental elastomers are described. The tread wear rate is discussed in relation to the slip ratio during braking and yaw angle during cornering. The extent of wear in either operational mode is examined in relation to the runway surface.
languageEnglish
titleNASA-TP-1569num
titleWear, friction, and temperature characteristics of an aircraft tire undergoing braking and corneringen
typestandard
page41
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1979
contenttypefulltext
subject keywordsAIRCRAFT TIRES
subject keywordsBRAKING
subject keywordsCOEFFICIENT OF FRICTION
subject keywordsELASTOMERS
subject keywordsKINETIC FRICTION
subject keywordsSURFACE TEMPERATURE
subject keywordsTREADS
subject keywordsWEAR TESTS


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