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Improved Computational Efficiency of Unsteady Flow Problems via the Modified Wavelet Method
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Kang, Hyung Min | - |
dc.contributor.author | Lee, Dong Ho | - |
dc.contributor.author | Kim, Kyu Hong | - |
dc.contributor.author | Lee, Do Hyung | - |
dc.date.accessioned | 2009-08-05T23:14:33Z | - |
dc.date.available | 2009-08-05T23:14:33Z | - |
dc.date.issued | 2008-05 | - |
dc.identifier.citation | AIAA Journal, vol.46, no.5, pp.1191-1203 | en |
dc.identifier.issn | 0001-1452 | - |
dc.identifier.uri | https://hdl.handle.net/10371/6213 | - |
dc.description.abstract | A newly modified adaptive wavelet method is proposed to enhance the computational efficiency and to maintain a level of accuracy in unsteady flow calculations that is similar to the conventional schemes. The slim and compressed data set is well adapted to the local features of a solution, and fluxes are only calculated according to this adaptive data set, which results in shorter total computation time. While retaining this advantage, the following methods are applied to the wavelet method. First, residual interpolation is applied and entire residual values are calculated before time integration, and it is therefore not necessary to add several cells to a data set, which were definitely necessary in previous wavelet methods. Second, the threshold value is modified to consider the temporal accuracy as well as the spatial accuracy of the conventional schemes. This modification ensures that the errors caused by the thresholding method do not damage the numerical accuracy of the conventional schemes. The modified wavelet method is successfully applied to the unsteady flow problems and compared with the results of the conventional solvers. In consequence, computing efficiency is enhanced without the deterioration of the solution accuracy. | en |
dc.description.sponsorship | The authors gratefully acknowledge that this research was
supported by the Brain Korea 21 program for the Mechanical and Aerospace Engineering Research at Seoul National University, by the Center of Innovative Design Optimization Technology, Korea Science and Engineering Foundation and by grant R01-2006-000- 10034-0 from the Basic Research Program of the Korea Science and Engineering Foundation. Also the authors gratefully acknowledge the financial support by the Agency for Defense Development and by the Flight Vehicle Research Center (FVRC), Seoul National University. | en |
dc.language.iso | en | - |
dc.publisher | American Institute of Aeronautics and Astronautics | en |
dc.subject | Numerical stability | en |
dc.subject | Computation time | en |
dc.subject | Digital simulation | en |
dc.subject | Modeling | en |
dc.subject | Computational fluid dynamics | en |
dc.subject | Wavelet transforms | en |
dc.subject | Adaptive method | en |
dc.subject | Interactions | en |
dc.subject | Finite volume methods | en |
dc.subject | Vortices | en |
dc.subject | Shock waves | en |
dc.subject | Unsteady flow | en |
dc.title | Improved Computational Efficiency of Unsteady Flow Problems via the Modified Wavelet Method | en |
dc.type | Article | en |
dc.contributor.AlternativeAuthor | 강형민 | - |
dc.contributor.AlternativeAuthor | 이동호 | - |
dc.contributor.AlternativeAuthor | 김규홍 | - |
dc.contributor.AlternativeAuthor | 이도형 | - |
dc.identifier.doi | 10.2514/1.34294 | - |
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