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EXPERIMENTAL STUDY ON THE MECHANISM OF THE RICHTMYERMESHKOV INSTABILITY AT A GAS-LIQUID INTERFACE 被引量:4

EXPERIMENTAL STUDY ON THE MECHANISM OF THE RICHTMYERMESHKOV INSTABILITY AT A GAS-LIQUID INTERFACE
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摘要 The mechanism of the Richtmyer-Meshkov instability was experimentally studied in a vertical rectangular shock tube. The velocity of the interface driven by the shock wave was measured by a self-designed measurement system, which consists of semiconductor lasers, signal amplification circuits, digital oscilloscope and computer. Tests were carded out at several shock wave Mach numbers. In addition, the movement of the interface and the variation of the mixed zone width with time were recorded by high-speed photography. The experimental results show that the interface velocity increases with the increase of the Mach number, and the distance of the interface's movement and the width of the mixed zone vary with time in a linear relationship. The mechanism of the Richtmyer-Meshkov instability was experimentally studied in a vertical rectangular shock tube. The velocity of the interface driven by the shock wave was measured by a self-designed measurement system, which consists of semiconductor lasers, signal amplification circuits, digital oscilloscope and computer. Tests were carded out at several shock wave Mach numbers. In addition, the movement of the interface and the variation of the mixed zone width with time were recorded by high-speed photography. The experimental results show that the interface velocity increases with the increase of the Mach number, and the distance of the interface's movement and the width of the mixed zone vary with time in a linear relationship.
出处 《Journal of Hydrodynamics》 SCIE EI CSCD 2009年第3期423-428,共6页 水动力学研究与进展B辑(英文版)
基金 supported by the National Natural Science Foundation of China (Grant No. 10672144) the Natural Science Foundation of Zhejiang Province (Grant No. Y107073)
关键词 Richtmyer-Meshkov instability shock wave shock tube LASER INTERFACE Richtmyer-Meshkov instability, shock wave, shock tube, laser, interface
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  • 1[1]POLIZER J L, KING W F III. Hydrodynamics of explosively generated high-velocity fluid jets. J. Appl. Phys., 1971, 42:2095-2099.
  • 2[2]AVDIENKO A A. Experimental estimation of different parameters effects on the fragmentation of viscoelastic liquid column ejected from circular channel by compressed gas. Inzhenerno-Fizicheskii Zhurnal, 1994, 66(1):24-29.
  • 3[3]BELLHOUSE B J, QUINLAN N J, AINSWORTH R W. Needle-less delivery of drugs, in dry powder form, using shock waves and supersonic gas flow, In: Proc 21st Int Symp Shock Waves, Paper 9555, 1997.
  • 4[4]SHI H H, WANG X L, ITOH M, KISHIMOTO M. Acceleration of water column and generation of large flow rate water spray by shock tube. JSME Int. J. Ser. B, 2001, 44(4): 543-551.
  • 5[5]WANG X L, SHI H H, ITOH M, KISHIMOTO M. Flow visualization of high speed liquid jet. In: Proc 24th Int. Congress High-Speed Photograph Photonics & Exhibitions, SPIE Vol. 4183, 2001, pp.899-906.
  • 6[6]WANG X L, ITOH M, SHI H H, KISHIMOTO M. Experimental study of Rayleigh-Taylor instability in a shock tube accompanying cavity formation. Jpn. J. Appl. Phys., 2001, 40(11):6668-6674.
  • 7[7]SHI H H, WANG X L. Hydrodynamic shock tube for quick transportation of spray with large flow rate. Exp. Fluids, 2002, 32(2):280-282.
  • 8[8]DUNNE B, CASSEN B. Velocity discontinuity instability of a liquid jet. J. Appl. Phys., 1956, 27:577-582.
  • 9[9]LEFEBVRE A H. Atomization and Sprays. Hemisphere publishing corporation, New York, 1989.
  • 10[10]SHI H H, YU M Z, CAI Y N. Investigation on the shock-wave velocity and impact pressure in high-speed impact on deformable media. In: Multiphase Transport and Particulate Phenomena, edited by T. N. Veziroglu, Hemisphere, New York, 1990, pp.567-580.

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