Abstract
A new mode matching method is developed for acoustic modes in axially sectioned lined ducts with parallel, but otherwise arbitrary mean flow. The method is evaluated in detail for radially symmetric mean flow, with so-called Pridmore-Brown modes, satisfying the radial Pridmore-Brown equation. Classically, the matching of the modal representations at the interfaces between the sections is based on continuity of pressure and velocity in combination with projection to a suitable but unrelated set of test functions by means of a standard integral inner-product. The alternative we propose here uses essentially the same Pridmore-Brown modes but instead of the standard inner-product we apply a particular bilinear form that can be evaluated in closed form. Apart from numerical efficiency, this approach features also a higher accuracy because it avoides the inherently inaccurate numerical quadrature of oscillating functions. The results are compared with results obtained by an implementation of the classical approach, and the agreement is excellent, with higher accuracy and with greater computational efficiency.
Original language | English |
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Title of host publication | 19th AIAA/CEAS Aeroacoustics Conference (Berlin, Germany, May 27-29, 2013) |
Publisher | American Institute of Aeronautics and Astronautics Inc. (AIAA) |
Number of pages | 21 |
ISBN (Print) | 978-162410213-4 |
DOIs | |
Publication status | Published - 2013 |
Event | 19th AIAA/CEAS Aeroacoustics Conference - Berlin, Germany Duration: 27 May 2013 → 29 May 2013 |
Conference
Conference | 19th AIAA/CEAS Aeroacoustics Conference |
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Country/Territory | Germany |
City | Berlin |
Period | 27/05/13 → 29/05/13 |