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Design and Test of Fan/Nacelle Models Quiet High-Speed FanThe Quiet High-Speed Fan program is a cooperative effort between Honeywell Engines & Systems (formerly AlliedSignal Engines & Systems) and the NASA Glenn Research Center. Engines & Systems has designed an advanced high-speed fan that will be tested on the Ultra High Bypass Propulsion Simulator in the NASA Glenn 9 x 15 foot wind tunnel, currently scheduled for the second quarter of 2000. An Engines & Systems modern fan design will be used as a baseline. A nacelle model is provided that is characteristic of a typical, modern regional aircraft nacelle and meets all of the program test objectives.
Document ID
20030068102
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Miller, Christopher J. (NASA Glenn Research Center Cleveland, OH, United States)
Weir, Donald (Honeywell Engines, Systems and Services Phoenix, AZ, United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2003
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-13946
NASA/CR-2003-212370
NAS 1.26:212370
Report Number: E-13946
Report Number: NASA/CR-2003-212370
Report Number: NAS 1.26:212370
Funding Number(s)
CONTRACT_GRANT: NAS3-27752
WORK_UNIT: WU-781-30-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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