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NASA-TN-D-7815

Experimental investigation of the cornering characteristics of 18 x 5.5, type 7, aircraft tires with different tread patterns

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1974

Abstract: The characteristics, which include the cornering-force and drag-force friction coefficients and self-alining torque, were obtained on dry, damp, and flooded runway surfaces over a range of yaw angles from 0 deg to 12 deg and at ground speeds from approximately 5 to 90 knots. The results indicate that a tread pattern with pinholes in the ribs reduces the tire cornering capability at high yaw angles on a damp surface but improves cornering on a dry surface. A tread pattern which has transverse grooves across the entire width of the tread improves the tire cornering performance slightly at high speeds on the flooded runway surface. The cornering capability of all the tires is degraded at high ground speeds by thin film lubrication and/or tire hydroplaning effects. Alterations to the conventional tread pattern provide only marginal improvements in the tire cornering capability which suggests that runway surface treatments may be a more effective way of improving aircraft ground performance during wet operations.
URI: http://yse.yabesh.ir/std;query=autho1216177D9D40527369728F1ED52F014A/handle/yse/225006
Subject: AERODYNAMIC COEFFICIENTS
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    NASA-TN-D-7815

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:43:37Z
date available2017-09-04T18:43:37Z
date copyright01/01/1974
date issued1974
identifier otherAMBBFEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho1216177D9D40527369728F1ED52F014A/handle/yse/225006
description abstractThe characteristics, which include the cornering-force and drag-force friction coefficients and self-alining torque, were obtained on dry, damp, and flooded runway surfaces over a range of yaw angles from 0 deg to 12 deg and at ground speeds from approximately 5 to 90 knots. The results indicate that a tread pattern with pinholes in the ribs reduces the tire cornering capability at high yaw angles on a damp surface but improves cornering on a dry surface. A tread pattern which has transverse grooves across the entire width of the tread improves the tire cornering performance slightly at high speeds on the flooded runway surface. The cornering capability of all the tires is degraded at high ground speeds by thin film lubrication and/or tire hydroplaning effects. Alterations to the conventional tread pattern provide only marginal improvements in the tire cornering capability which suggests that runway surface treatments may be a more effective way of improving aircraft ground performance during wet operations.
languageEnglish
titleNASA-TN-D-7815num
titleExperimental investigation of the cornering characteristics of 18 x 5.5, type 7, aircraft tires with different tread patternsen
typestandard
page22
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1974
contenttypefulltext
subject keywordsAERODYNAMIC COEFFICIENTS
subject keywordsAIRCRAFT TIRES
subject keywordsFRICTION DRAG
subject keywordsHYDROPLANING
subject keywordsRUNWAY CONDITIONS
subject keywordsSELF ALIGNMENT
subject keywordsTORQUE
subject keywordsTRACTION
subject keywordsTREADS
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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
yabeshDSpacePersian