Presentation 2008-04-11
Study of Application of Compressible Flow and Shock Wave to PLA
Minoru YAGA, Hiroshi FUKUOKA, Hideki MINE, Toshio TAKIYA,
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Abstract(in English) The unsteady behavior of flow driven by a jet suddenly injected into a cell is numerically studied by solving the axisymmetric two-dimensional compressible Navier-Stokes equations. This system of the calculation is a model of the laser ablation of a certain duration followed by a discharging process through the exit hole at the downstream end of the cell. As the result, it was found that the number of the peaks and the maximum velocity downstream of the cell exit are roughly determined by the focal point of the elliptical cell.
Keyword(in Japanese) (See Japanese page)
Keyword(in English) Shock Wave / CFD / Supersonic Flow / Unsteady jet / Velocity variation
Paper # SDM2008-2,OME2008-2
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Committee OME
Conference Date 2008/4/4(1days)
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Registration To Organic Material Electronics (OME)
Language JPN
Title (in Japanese) (See Japanese page)
Sub Title (in Japanese) (See Japanese page)
Title (in English) Study of Application of Compressible Flow and Shock Wave to PLA
Sub Title (in English)
Keyword(1) Shock Wave
Keyword(2) CFD
Keyword(3) Supersonic Flow
Keyword(4) Unsteady jet
Keyword(5) Velocity variation
1st Author's Name Minoru YAGA
1st Author's Affiliation University of the Ryukyus()
2nd Author's Name Hiroshi FUKUOKA
2nd Author's Affiliation University of the Ryukyus
3rd Author's Name Hideki MINE
3rd Author's Affiliation University of the Ryukyus
4th Author's Name Toshio TAKIYA
4th Author's Affiliation Hitachi Zosen Corporation
Date 2008-04-11
Paper # SDM2008-2,OME2008-2
Volume (vol) vol.108
Number (no) 2
Page pp.pp.-
#Pages 4
Date of Issue