Study of Unsteady Supersonic Jet Using Shock Tube with Small High-Pressure Chamber with Elliptical Cell

Motoki Sakamoto; Masazumi Matsui; Hiroshi Fukuoka; Minoru Yaga; Toshio Takiya

doi:10.4028/www.scientific.net/MSF.767.80

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HomeMaterials Science ForumMaterials Science Forum Vol. 767Study of Unsteady Supersonic Jet Using Shock Tube...

Study of Unsteady Supersonic Jet Using Shock Tube with Small High-Pressure Chamber with Elliptical Cell

Abstract:

The unsteady supersonic jet formed by the shock tube with small high-pressure chamber was used as a simple alternative model of Pulsed laser ablation. Since the pressure of the shock wave formed by Pulsed laser ablation is very high, the interaction between the shock wave and the plume is important for the formation of nanoparticles especially under high background gas pressure. An elliptical cell is used for controlling the shock wave. The shock wave discharged in one focal point converge another focal point. Numerical calculation was carried out by solving the axisymmetric two-dimensional compressible Navier-Stokes equations. The wall static pressure monitored at the center of substrate is used to evaluate the influence of the shape and the pressure ratio on the behavior of the shock wave, the plume, and their interaction. As a result, it was found that the vortex ring was generated downstream of the cell, which is followed by the discharging shock wave from the cell exit. It was also found that the influence of the vortex ring on the wall static pressure at the center of the substrate.

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Periodical:

Materials Science Forum (Volume 767)

Pages:

80-85

DOI:

https://doi.org/10.4028/www.scientific.net/MSF.767.80

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Cite this paper

Online since:

July 2013

Authors:

Motoki Sakamoto, Masazumi Matsui, Hiroshi Fukuoka, Minoru Yaga, Toshio Takiya

Keywords:

Computational Fluid Dynamics (CFD), Elliptical Cell, Shock Wave, Unsteady Jet

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References

[1] Umezu, I., Yamamoto, S., Sugimura, A., Emission induced by collision of two plumes during pulsed laser ablation, Appl. Phys. A, 101 (2010) 133-136.

DOI: 10.1007/s00339-010-5772-3

Google Scholar

[2] Seto, T., Orii, T., Hirasawa, M., Aya, N., Fabrication of silicon nanostructured films by deposition of size-selected nanoparticles generated by pulsed laser ablation, Thin Solid Films, 437 (2003) 230-234.

DOI: 10.1016/s0040-6090(02)00732-0

Google Scholar

[3] Naono, Y., Kawabata, S., Huh, S.H., Nakajima, A., Classification and characterization of gold and nickel nanoparticles with a differential mobility analyzer, Science and Technology of Advanced Materials, 7 (2006) 209-215.

DOI: 10.1016/j.stam.2005.11.025

Google Scholar

[4] Iwata, Y., Kishida, M., Muto, M., Yu, S., Sawada, T., Fukuda, A., Takiya, T., Komura, A. and Nakajima, K., Narrow size-distributed silicon cluster beam generated using a spatiotemporal confirned cluster source, Chem. Phys. Lett., 358 (2002) 36-42.

DOI: 10.1016/s0009-2614(02)00556-0

Google Scholar

[5] Yaga, M., Takiya, T., Iwata, Y., Numerical study of unsteady compressible flow driven by supersonic jet injected into elliptical cell with small exit hole, Shock waves, 14 (2005) 403-411.

DOI: 10.1007/s00193-005-0278-1

Google Scholar