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The effect of chine tires on nose gear water-spray characteristics of a twin engine airplaneAn 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.
Document ID
19750015483
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Yager, T. J.
(NASA Langley Research Center Hampton, VA, United States)
Stubbs, S. M.
(NASA Langley Research Center Hampton, VA, United States)
Mccarty, J. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-X-72695
Accession Number
75N23555
Funding Number(s)
PROJECT: RTOP 505-08-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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