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Noise Prediction Module for Offset Stream NozzlesA Modern Design of Experiments (MDOE) analysis of data acquired for an offset stream technology was presented. The data acquisition and concept development were funded under a Supersonics NRA NNX07AC62A awarded to Dimitri Papamoschou at University of California, Irvine. The technology involved the introduction of airfoils in the fan stream of a bypass ratio (BPR) two nozzle system operated at transonic exhaust speeds. The vanes deflected the fan stream relative to the core stream and resulted in reduced sideline noise for polar angles in the peak jet noise direction. Noise prediction models were developed for a range of vane configurations. The models interface with an existing ANOPP module and can be used or future system level studies.
Document ID
20110008760
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Henderson, Brenda S.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
March 15, 2011
Subject Category
Acoustics
Report/Patent Number
E-17739
Meeting Information
Meeting: 2011 Technical Conference, NASA Fundamental Aeronautics Program
Location: Cleveland, OH
Country: United States
Start Date: March 15, 2011
End Date: March 17, 2011
Funding Number(s)
CONTRACT_GRANT: NNX07AC62A
WBS: WBS 98474.02.07.03.17.08.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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