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Flow Rate and Trajectory of Water Spray Produced by an Aircraft Tire NASA Langley Research Center

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Daughterly, Robert H., author.
Conference Name:
SAE Aerospace Technology Conference and Exposition (1986-10-13 : Long Beach, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1986
Summary:
One of the risks associated with wet runway aircraft operation is the ingestion of water spray produced by an aircraft's tires into its engines. This problem can be especially dangerous at or near rotation speed on the takeoff roll. An experimental investigation was conducted in the NASA Langley Research Center Hydrodynamics Research Facility to measure the flow rate and trajectory of water spray produced by an aircraft nose tire operating on a flooded runway. The effects of various parameters on the spray patterns including distance aft of nosewheel, speed, load, and water depth were evaluated. Variations in the spray pattern caused by the airflow about primary structure such as the fuselage and wing are discussed. A discussion of events in and near the tire footprint concerning spray generation is included
Notes:
Vendor supplied data
Publisher Number:
861626
Access Restriction:
Restricted for use by site license

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