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Applications of velocity potential function to acoustic duct propagation and radiation from inlets using finite element theoryA finite element velocity potential program was developed to study acoustic wave propagation in complex geometries. For irrotational flows, relatively low sound frequencies, and plane wave input, the finite element solutions showed significant effects of inlet curvature and flow gradients on the attenuation of a given acoustic liner in a realistic variable area turbofan inlet. The velocity potential approach can not be used to estimate the effects of rotational flow on acoustic propagation, since the potential acoustic disturbances propagate at the speed of the media in sheared flow. Approaches are discussed that are being considered for extending the finite element solution to include the far field, as well as the internal portion of the duct. A new matrix partitioning approach is presented that can be incorporated in previously developed programs to allow the finite element calculation to be marched into the far field. The partitioning approach provided a large reduction in computer storage and running times.
Document ID
19790007788
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baumeister, K. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Majjigi, R. K.
(GE Co. Cincinnati, Ohio, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1979
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-79071
E-9888
Report Number: NASA-TM-79071
Report Number: E-9888
Meeting Information
Meeting: Aeroacoustics Conf.
Location: Seattle, WA
Country: United States
Start Date: March 12, 1979
End Date: March 14, 1979
Sponsors: AIAA
Accession Number
79N15959
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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