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Turbofan Duct Propagation ModelThe CDUCT code utilizes a parabolic approximation to the convected Helmholtz equation in order to efficiently model acoustic propagation in acoustically treated, complex shaped ducts. The parabolic approximation solves one-way wave propagation with a marching method which neglects backwards reflected waves. The derivation of the parabolic approximation is presented. Several code validation cases are given. An acoustic lining design process for an example aft fan duct is discussed. It is noted that the method can efficiently model realistic three-dimension effects, acoustic lining, and flow within the computational capabilities of a typical computer workstation.
Document ID
20020030747
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Lan, Justin H.
(Boeing Co. Seattle, WA United States)
Posey, Joe W.
Date Acquired
September 7, 2013
Publication Date
December 1, 2001
Subject Category
Acoustics
Report/Patent Number
NAS 1.26:211245
NASA/CR-2001-211245
Report Number: NAS 1.26:211245
Report Number: NASA/CR-2001-211245
Funding Number(s)
CONTRACT_GRANT: NAS1-97040
PROJECT: RTOP 706-81-12-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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