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Improved Computational Efficiency of Unsteady Flow Problems via the Modified Wavelet Method

DC Field Value Language
dc.contributor.authorKang, Hyung Min-
dc.contributor.authorLee, Dong Ho-
dc.contributor.authorKim, Kyu Hong-
dc.contributor.authorLee, Do Hyung-
dc.date.accessioned2009-08-05T23:14:33Z-
dc.date.available2009-08-05T23:14:33Z-
dc.date.issued2008-05-
dc.identifier.citationAIAA Journal, vol.46, no.5, pp.1191-1203en
dc.identifier.issn0001-1452-
dc.identifier.urihttps://hdl.handle.net/10371/6213-
dc.description.abstractA 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.sponsorshipThe 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.isoen-
dc.publisherAmerican Institute of Aeronautics and Astronauticsen
dc.subjectNumerical stabilityen
dc.subjectComputation timeen
dc.subjectDigital simulationen
dc.subjectModelingen
dc.subjectComputational fluid dynamicsen
dc.subjectWavelet transformsen
dc.subjectAdaptive methoden
dc.subjectInteractionsen
dc.subjectFinite volume methodsen
dc.subjectVorticesen
dc.subjectShock wavesen
dc.subjectUnsteady flowen
dc.titleImproved Computational Efficiency of Unsteady Flow Problems via the Modified Wavelet Methoden
dc.typeArticleen
dc.contributor.AlternativeAuthor강형민-
dc.contributor.AlternativeAuthor이동호-
dc.contributor.AlternativeAuthor김규홍-
dc.contributor.AlternativeAuthor이도형-
dc.identifier.doi10.2514/1.34294-
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