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Progress towards a new computational scheme for aeroacoustics

Publication ,  Conference
Thomas, JP; Kim, C; Roe, PL
Published in: 12th Computational Fluid Dynamics Conference
January 1, 1995

© 1995 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.To develop numerical schemes for aeroacoustics, numerical techniques based upon the upwind leapfrog method have been devised and tested on some model problems. Fourth-order variations of the upwind leapfrog scheme are studied and methods for applying these schemes to equations with source terms and non-constant coefficients are developed. Additionally, extensions of these upwind leapfrog ideas to the multi-dimensional ad- vection equation and the acoustic system of equations in stationary and uniform flows are studied.

Duke Scholars

Published In

12th Computational Fluid Dynamics Conference

ISBN

9780000000002

Publication Date

January 1, 1995

Start / End Page

1325 / 1338
 

Citation

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Thomas, J. P., Kim, C., & Roe, P. L. (1995). Progress towards a new computational scheme for aeroacoustics. In 12th Computational Fluid Dynamics Conference (pp. 1325–1338).
Thomas, J. P., C. Kim, and P. L. Roe. “Progress towards a new computational scheme for aeroacoustics.” In 12th Computational Fluid Dynamics Conference, 1325–38, 1995.
Thomas JP, Kim C, Roe PL. Progress towards a new computational scheme for aeroacoustics. In: 12th Computational Fluid Dynamics Conference. 1995. p. 1325–38.
Thomas, J. P., et al. “Progress towards a new computational scheme for aeroacoustics.” 12th Computational Fluid Dynamics Conference, 1995, pp. 1325–38.
Thomas JP, Kim C, Roe PL. Progress towards a new computational scheme for aeroacoustics. 12th Computational Fluid Dynamics Conference. 1995. p. 1325–1338.
Journal cover image

Published In

12th Computational Fluid Dynamics Conference

ISBN

9780000000002

Publication Date

January 1, 1995

Start / End Page

1325 / 1338