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NASA-TM-X-72695

The effect of chine tires on nose gear water-spray characteristics of a twin engine airplane

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1975

Abstract: An experimental investigation was performed to evaluate the effectiveness of nose gear chine tires in eliminating or minimizing the engine spray ingestion problem encountered on several occasions by the Merlin 4, a twin-engine propjet airplane. A study of the photographic and television coverage indicated that under similar test conditions the spray from the chine tires presented less of a potential engine spray ingestion problem than the conventional tires. Neither tire configuration appeared to pose any ingestion problem at aircraft speeds in excess of the hydroplaning speed for each tire, however, significant differences were noted in the spray patterns of the two sets of tires at sub-hydroplaning speeds. At sub-hydroplaning speeds, the conventional tires produced substantial spray above the wing which approached the general area of the engine air inlet at lower test speeds. The chine tires produced two distinct spray plumes at sub-hydroplaning speeds: one low-level plume which presented no apparent threat of ingestion, and one which at most test speeds was observed to be below the wing leading edge and thus displaced from the intakes on the engine nacelle.
URI: https://yse.yabesh.ir/std/handle/yse/98299
Subject: AIRCRAFT HAZARDS
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    NASA-TM-X-72695

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:34:46Z
date available2017-09-04T16:34:46Z
date copyright01/01/1975
date issued1975
identifier otherUYHOEEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/98299
description abstractAn experimental investigation was performed to evaluate the effectiveness of nose gear chine tires in eliminating or minimizing the engine spray ingestion problem encountered on several occasions by the Merlin 4, a twin-engine propjet airplane. A study of the photographic and television coverage indicated that under similar test conditions the spray from the chine tires presented less of a potential engine spray ingestion problem than the conventional tires. Neither tire configuration appeared to pose any ingestion problem at aircraft speeds in excess of the hydroplaning speed for each tire, however, significant differences were noted in the spray patterns of the two sets of tires at sub-hydroplaning speeds. At sub-hydroplaning speeds, the conventional tires produced substantial spray above the wing which approached the general area of the engine air inlet at lower test speeds. The chine tires produced two distinct spray plumes at sub-hydroplaning speeds: one low-level plume which presented no apparent threat of ingestion, and one which at most test speeds was observed to be below the wing leading edge and thus displaced from the intakes on the engine nacelle.
languageEnglish
titleNASA-TM-X-72695num
titleThe effect of chine tires on nose gear water-spray characteristics of a twin engine airplaneen
typestandard
page26
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1975
contenttypefulltext
subject keywordsAIRCRAFT HAZARDS
subject keywordsAIRCRAFT TIRES
subject keywordsAIRFIELD SURFACE MOVEMENTS
subject keywordsLANDING GEAR
subject keywordsNOSE WHEELS
subject keywordsOPERATIONS RESEARCH
subject keywordsRUNWAY CONDITIONS
subject keywordsSPRAY INGESTION
subject keywordsWATER
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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