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Computed Linear/Nonlinear Acoustic Response of a Cascade for Single/Multi Frequency ExcitationThis paper examines mode generation and propagation characteristics of a 2-D cascade due to incident vortical disturbances using a time domain approach. Full nonlinear Euler equations are solved employing high order accurate spatial differencing and time marching techniques. The solutions show the generation and propagation of mode orders that are expected from theory. Single frequency excitations show linear response over a wide range of amplitudes. The response for multi-frequency excitations tend to become nonlinear due to interaction between frequencies and self interaction.
Document ID
20040082396
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Nallasamy, M.
(QSS Group, Inc. Cleveland, OH, United States)
Hixon, R.
(Toledo Univ. OH, United States)
Sawyer, S.
(Akron Univ. Akron, OH, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2004
Subject Category
Aeronautics (General)
Report/Patent Number
NASA/CR-2004-213110
E-14584
AIAA Paper 2004-2998
Report Number: NASA/CR-2004-213110
Report Number: E-14584
Report Number: AIAA Paper 2004-2998
Meeting Information
Meeting: Tenth Aeroacoustics Conference
Location: Manchester
Country: United Kingdom
Start Date: May 10, 2004
End Date: May 12, 2004
Sponsors: Confederation of European Aerospace Societies, American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS3-00145
WBS: WBS 781-30-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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