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The Aerodynamic Performance of an Over-the-Rotor Liner with Circumferential Grooves on a High Bypass Ratio Turbofan RotorNo abstract available
Document ID
20150007668
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Bozak, Rick (NASA Glenn Research Center Cleveland, OH, United States)
Hughes, Christopher (NASA Glenn Research Center Cleveland, OH, United States)
Buckley, James (Vantage Partners, LLC Brook Park, OH, United States)
Date Acquired
May 7, 2015
Publication Date
June 3, 2013
Subject Category
Aircraft Design, Testing And Performance
Aerodynamics
Aircraft Propulsion And Power
Report/Patent Number
E-664020
Meeting Information
Meeting: ASME Turbo Expo 2013 (TE2013)
Location: San Antonio, TX
Country: United States
Start Date: June 3, 2013
End Date: June 7, 2013
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 699959.02.09.03.06
Distribution Limits
Public
Copyright
Public Use Permitted.

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