NASA NTRS · 19970029055
Solution of Aeroacoustic Problems by a Nonlinear, Hybrid Method
Abstract
Category 1, problem 3 (scattering of sound by a sphere) and category 2, problem 1 (spherical source in a cylindrical duct subject to uniform flow) are solved in generalized coordinates using the nonlinear Euler equations together with nonreflecting boundary conditions. A temporally and spatially fourth-order accurate finite-difference, Runge-Kutta time-marching technique is employed for the near-field calculations and a Kirchhoff method is employed for the prediction of far-field sound. Computations are all performed on parallel processors using the data-parallel paradigm.
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Oezyoeruek, Yusuf, Long, Lyle N.. 1997-06-01. Solution of Aeroacoustic Problems by a Nonlinear, Hybrid Method. https://ntrs.nasa.gov/citations/19970029055
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