4th AIAA/CEAS Aeroacoustics Conference 1998
DOI: 10.2514/6.1998-2309
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Modal conversion from untreated to treated cylindrical ducts

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Cited by 2 publications
(1 citation statement)
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“…Eversman and Cook 4 changed the eigenvalue equation into a differential one which can be integrated by using the Runge-Kutta algorithm. Montetagaud et al 5 used this method with a more precise step. Rienstra 6 identified the modes in ducts in two categories: The duct modes resulting from the finiteness of the duct geometry, and the surface waves that exist only near the wall surface in a way essentially independent of the rest of the duct.…”
Section: Introductionmentioning
confidence: 98%
“…Eversman and Cook 4 changed the eigenvalue equation into a differential one which can be integrated by using the Runge-Kutta algorithm. Montetagaud et al 5 used this method with a more precise step. Rienstra 6 identified the modes in ducts in two categories: The duct modes resulting from the finiteness of the duct geometry, and the surface waves that exist only near the wall surface in a way essentially independent of the rest of the duct.…”
Section: Introductionmentioning
confidence: 98%