Progress towards a new computational scheme for aeroacoustics
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Thomas, JP; Kim, C; Roe, PL
Published in: 12th Computational Fluid Dynamics Conference
January 1, 1995
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
DOI
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). https://doi.org/10.2514/6.1995-1758
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. https://doi.org/10.2514/6.1995-1758.
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. Scopus, doi:10.2514/6.1995-1758.
Thomas JP, Kim C, Roe PL. Progress towards a new computational scheme for aeroacoustics. 12th Computational Fluid Dynamics Conference. 1995. p. 1325–1338.
Published In
12th Computational Fluid Dynamics Conference
DOI
Publication Date
January 1, 1995
Start / End Page
1325 / 1338