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NASA-TN-D-6964

An evaluation of some unbraked tire cornering force characteristics

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1972

Abstract: An investigation to determine the effects of pavement surface condition on the cornering forces developed by a group of 6.50x13 automobile tires of different tread design was conducted at the Langley aircraft landing loads and traction facility. The tests were made at fixed yaw angles of 3,4.5, and 6 deg at forward speeds up to 80 knots on two concrete surfaces of different texture under dry, damp, and flooded conditions. The results showed that the cornering forces were extremely sensitive to tread pattern and runway surface texture under all conditions and that under flooded conditions tire hydroplaning and complete loss of cornering force occurred at a forward velocity predicted from an existing formula based on tire inflation pressure. Futher, tests on the damp concrete with a smooth tire and a four-groove tire showed higher cornering forces at a yaw angle of 3 deg than at 4.5 deg; this indicated that maximum cornering forces are developed at extremely small steering angles under these conditions.
URI: http://yse.yabesh.ir/std/handle/yse/141466
Subject: LOADS (FORCES)
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    NASA-TN-D-6964

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:18:06Z
date available2017-09-04T17:18:06Z
date copyright01/01/1972
date issued1972
identifier otherZKBBFEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/141466
description abstractAn investigation to determine the effects of pavement surface condition on the cornering forces developed by a group of 6.50x13 automobile tires of different tread design was conducted at the Langley aircraft landing loads and traction facility. The tests were made at fixed yaw angles of 3,4.5, and 6 deg at forward speeds up to 80 knots on two concrete surfaces of different texture under dry, damp, and flooded conditions. The results showed that the cornering forces were extremely sensitive to tread pattern and runway surface texture under all conditions and that under flooded conditions tire hydroplaning and complete loss of cornering force occurred at a forward velocity predicted from an existing formula based on tire inflation pressure. Futher, tests on the damp concrete with a smooth tire and a four-groove tire showed higher cornering forces at a yaw angle of 3 deg than at 4.5 deg; this indicated that maximum cornering forces are developed at extremely small steering angles under these conditions.
languageEnglish
titleNASA-TN-D-6964num
titleAn evaluation of some unbraked tire cornering force characteristicsen
typestandard
page39
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1972
contenttypefulltext
subject keywordsLOADS (FORCES)
subject keywordsPERFORMANCE TESTS
subject keywordsSTRESS ANALYSIS
subject keywordsSURFACE ROUGHNESS
subject keywordsTEST EQUIPMENT
subject keywordsTIRES
subject keywordsTRACTION
subject keywordsVEHICLE WHEELS
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DSpace software copyright © 2017-2020  DuraSpace
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