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NASA-TP-1080

Friction characteristics of three 30 X 11.5-14.5, type 8, aircraft tires with various tread groove patterns and rubber compounds

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1977

Abstract: A test program was conducted to evaluate friction performance and wear characteristics on wet runways of three 30 x 11.5-14.5, type, aircraft tires having two different tread patterns and natural rubber contents. All test tires had the standard three circumferential groove tread, but two had molded transverse grooves which extended from shoulder to shoulder. The tread rubber content of the two tires with transverse grooves differed in that one had a 100 percent natural rubber tread and the other had a rubber tread composition that was 30 percent synthetic and 70 percent natural. The third test tire had the conventional 100 percent natural rubber tread. Results indicate that the differences in tire tread design and rubber composition do not significantly affect braking and cornering friction capability on wet or dry surfaces. Braking performance of the tires decreases with increased speed, with increased yaw angle and, at higher speeds, with increased wetness of the surface.
URI: https://yse.yabesh.ir/std/handle/yse/74620
Subject: AIRCRAFT LANDING
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    NASA-TP-1080

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:11:23Z
date available2017-09-04T16:11:23Z
date copyright01/01/1977
date issued1977
identifier otherSMBBFEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/74620
description abstractA test program was conducted to evaluate friction performance and wear characteristics on wet runways of three 30 x 11.5-14.5, type, aircraft tires having two different tread patterns and natural rubber contents. All test tires had the standard three circumferential groove tread, but two had molded transverse grooves which extended from shoulder to shoulder. The tread rubber content of the two tires with transverse grooves differed in that one had a 100 percent natural rubber tread and the other had a rubber tread composition that was 30 percent synthetic and 70 percent natural. The third test tire had the conventional 100 percent natural rubber tread. Results indicate that the differences in tire tread design and rubber composition do not significantly affect braking and cornering friction capability on wet or dry surfaces. Braking performance of the tires decreases with increased speed, with increased yaw angle and, at higher speeds, with increased wetness of the surface.
languageEnglish
titleNASA-TP-1080num
titleFriction characteristics of three 30 X 11.5-14.5, type 8, aircraft tires with various tread groove patterns and rubber compoundsen
typestandard
page27
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1977
contenttypefulltext
subject keywordsAIRCRAFT LANDING
subject keywordsAIRCRAFT TIRES
subject keywordsBRAKING
subject keywordsFRICTION MEASUREMENT
subject keywordsRUBBER
subject keywordsRUNWAYS
subject keywordsTREADS
subject keywordsWEAR TESTS
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DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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