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The Role of Analytic Methods in Computational AeroacousticsAs air traffic grows, annoyance produced by aircraft noise will grow unless new aircraft produce no objectionable noise outside airport boundaries. Such ultra-quiet aircraft must be of revolutionary design, having unconventional planforms and most likely with propulsion systems highly integrated with the airframe. Sophisticated source and propagation modeling will be required to properly account for effects of the airframe on noise generation, reflection, scattering, and radiation. It is tempting to say that since all the effects are included in the Navier-Stokes equations, time-accurate CFD can provide all the answers. Unfortunately, the computational time required to solve a full aircraft noise problem will be prohibitive for many years to come. On the other hand, closed form solutions are not available for such complicated problems. Therefore, a hybrid approach is recommended in which analysis is taken as far as possible without omitting relevant physics or geometry. Three examples are given of recently reported work in broadband noise prediction, ducted fan noise propagation and radiation, and noise prediction for complex three-dimensional jets.
Document ID
20040001059
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Farassat, F.
(NASA Langley Research Center Hampton, VA, United States)
Posey, J. W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Aerodynamics
Meeting Information
Meeting: Aerospace National Simulation Symposium 2003
Country: Unknown
Start Date: January 1, 2003
Funding Number(s)
OTHER: 23-781-10-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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