Low-Dispersion Finite Volume Scheme for Aeroacoustic Applications

The development ofa low-dispersion numerical scheme is described in the context of a finite volume discretization of the governing fluid dynamic equations. Although low-dispersion finite difference schemes have been developed recently for uniform Cartesian meshes, current finite volume methods do not possess low-dispersion characteristics. A low-dispersion finite volume scheme is presented and applied to some common acoustics problems. The two-dimensional unsteady Euler equations linearized about a mean flow are solved using a finite volume formulation. The surface integrals are computed using flow properties at cell faces, interpolated from cell nodes. The interpolation process is chosen such that it accurately represents sinusoidal waves of short wavelengths at the cell faces. A number of classical acoustics problems are solved, and where possible, comparisons with other numerical and exact solutions are given. This scheme has low dispersion and may be retrofitted easily into existing finite volume codes. The resulting numerical method combines the flexibility and versatility of the finite volume method while minimizing numerical dispersion errors in a manner similar to that of the classical dispersion-relation-preserving scheme.

[1]  B. V. Leer,et al.  Towards the ultimate conservative difference scheme V. A second-order sequel to Godunov's method , 1979 .

[2]  Jay C. Hardin,et al.  Regarding Numerical Considerations for Computational Aeroacoustics , 1993 .

[3]  K. Ahuja,et al.  Computational aeroacoustics as applied to the diffraction of sound by cylindrical bodies , 1986 .

[4]  Lakshmi N. Sankar,et al.  Toward the direct calculation of noise - Fluid/acoustic coupled simulation , 1995 .

[5]  P. Morse Vibration and Sound , 1949, Nature.

[6]  P. Sweby High Resolution Schemes Using Flux Limiters for Hyperbolic Conservation Laws , 1984 .

[7]  Allan D. Pierce,et al.  Acoustics , 1989 .

[8]  B. V. Leer,et al.  Towards the Ultimate Conservative Difference Scheme , 1997 .

[9]  C. Hirsch,et al.  Numerical Computation of Internal and External Flows. By C. HIRSCH. Wiley. Vol. 1, Fundamentals of Numerical Discretization. 1988. 515 pp. £60. Vol. 2, Computational Methods for Inviscid and Viscous Flows. 1990, 691 pp. £65. , 1991, Journal of Fluid Mechanics.

[10]  Christopher K. W. Tam,et al.  Dispersion-relation-preserving schemes for computational aeroacoustics , 1992 .

[11]  A. Lyrintzis Review: the use of Kirchhoff's method in computational aeroacoustics , 1994 .

[12]  J. Steger,et al.  Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods , 1981 .

[13]  G. Whitham,et al.  Linear and Nonlinear Waves , 1976 .

[14]  J. Hardin,et al.  Sound Generation by Flow over a Two-Dimensional Cavity , 1995 .

[15]  A. Jameson,et al.  Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes , 1981 .

[16]  Eli Turkel,et al.  Dissipative two-four methods for time-dependent problems , 1976 .

[17]  A third order upwind scheme for aero-acoustic applications , 1993 .

[18]  Christopher K. W. Tam,et al.  Computational aeroacoustics - Issues and methods , 1995 .

[19]  Lakshmi N. Sankar,et al.  A TECHNIQUE FOR THE PREDICTION OF PROPELLER INDUCED ACOUSTIC LOADS ON AIRCRAFT STRUCTURES , 1993 .

[20]  B. Leer,et al.  Flux-vector splitting for the Euler equations , 1997 .

[21]  C. Tam,et al.  Dispersion-relation-preserving finite difference schemes for computational acoustics , 1993 .