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Computational Aero-acoustics As a Tool For Turbo-machinery Noise ReductionThis talk will provide an overview of the field of computational aero-acoustics and its use in fan noise prediction. After a brief history of computational fluid dynamics, some of the recent developments in computational aero-acoustics will be explored. Computational issues concerning sound wave production, propagation, and reflection in practical turbo-machinery applications will be discussed including: (a) High order/High Resolution Numerical Techniques. (b) High Resolution Boundary Conditions. [c] MIMD Parallel Computing. [d] Form of Governing Equations Useful for Simulations. In addition, the basic design of our Broadband Analysis Stator Simulator (BASS) code and its application to a 2 D rotor wake-stator interaction will be shown. An example of the noise produced by the wakes from a rotor impinging upon a stator cascade will be shown.
Document ID
20030107838
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Dyson, Rodger W.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 21, 2013
Publication Date
April 25, 2003
Subject Category
Acoustics
Meeting Information
Meeting: Computational Aero-acoustics As a Tool For Turbo-machinery Noise Reduction
Location: Akron, OH
Country: United States
Start Date: April 18, 2003
Funding Number(s)
WBS: WBS 22-781-30-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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