A numerical method is developed for solving subsonic flows with convected, three-dimensional vortical waves around lifting airfoils. The first-order method that is presented fully accounts for the distortion effects of the nonuniform mean flow on the convected vorticity. The unsteady velocity is spl
Time-domain computation of muffler frequency response: Comparison of different numerical schemes
β Scribed by A. Broatch; J.R. Serrano; F.J. Arnau; D. Moya
- Publisher
- Elsevier Science
- Year
- 2007
- Tongue
- English
- Weight
- 284 KB
- Volume
- 305
- Category
- Article
- ISSN
- 0022-460X
No coin nor oath required. For personal study only.
β¦ Synopsis
A comparative study of the performance of different schemes used to solve one-dimensional gas flow equations when applied to the computation of the frequency response of exhaust mufflers is presented. Simple but representative systems with well-known acoustic behaviour were considered. Apart from the classical Lax-Wendroff and MacCormack schemes, the total variation diminishing schemes, flux corrected transport techniques or the innovative space-time conservation element and solution element method were considered. The results provide guidelines for a proper choice of the numerical scheme, taking into account the mesh spacing.
π SIMILAR VOLUMES
Parallel algorithms for the finite difference time-domain (FDTD), the planar generalized Yee (PGY), and the finite element time-domain (FETD) methods are presented. The FDTD and the PGY algorithms are both explicit time-domain solutions of Maxwell's equations, while the PGY algorithm is based on an
Earlier work\ using the time dependent Poynting theorem has shown that the complete description of power in a multimodal radiation "eld requires the use of three numbers; two are su$cient only with a single modal "eld. Where three numbers are required it is not possible to correctly represent power