NASA NTRS · 20020030747
Turbofan Duct Propagation Model
Abstract
The 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.
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Lan, Justin H., Posey, Joe W.. 2001-12-01. Turbofan Duct Propagation Model. https://ntrs.nasa.gov/citations/20020030747
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