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Multifunctional Low Pressure Turbine for Core Noise Reduction, Improved Efficiency, and NOx ReductionDetermining the feasibility of the induced synthetic jet is key, and is still TBD. center dot Available LPT vane volume is sufficient for tens of resonators per span-wise hole spacing, so physically feasible. center dot Determination of acoustic attenuation requires accurate model of vane, resonator locations, flow field and incident waves. (TBD) center dot Determination of NOx reduction is also TBD.
Document ID
20150007673
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Miller, Chris
(NASA Glenn Research Center Cleveland, OH, United States)
Shyam, Vikram
(NASA Glenn Research Center Cleveland, OH, United States)
Rigby, David
(Vantage Partners, LLC Brook Park, OH, United States)
Acosta, Waldo
Date Acquired
May 7, 2015
Publication Date
July 9, 2013
Subject Category
Fluid Mechanics And Thermodynamics
Aircraft Propulsion And Power
Report/Patent Number
E-664025
Report Number: E-664025
Funding Number(s)
WBS: WBS 694478.02.93.02.12
Distribution Limits
Public
Copyright
Public Use Permitted.
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