Volume 27 Issue 6
Jun.  2001
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DAI Qin, WEI Run-jie, HUANG Zhan, et al. Experimental Study of Supersonic Jet Flow Using DPIV[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(6): 666-669. (in Chinese)
Citation: DAI Qin, WEI Run-jie, HUANG Zhan, et al. Experimental Study of Supersonic Jet Flow Using DPIV[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(6): 666-669. (in Chinese)

Experimental Study of Supersonic Jet Flow Using DPIV

  • Received Date: 12 Apr 2000
  • Publish Date: 30 Jun 2001
  • Experimental study of supersonic jet flow using digital PIV system with frame straddle CCD camera is introduced in the paper. The diameter and Mach number of the Laval nozzle exit are 13.8mm and 1.5 respectively, the vector field and wave patterns of the jet flow in different pressure ratio of the stagnation pressure with the surrounding static pressure were observed. The results show the different of flow speed and other parameter of flow field before and after the shock wave. The generation of particles and seeding method are also simply described in the paper.

     

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  • [1] Alkislar M B,Lourenceo L, Krothapalli A. 3-D PIV measurements of a supersonic jet .Proc of the 3rd International Workshop on PIV'99 .CA,Santa Barbara, US:Univ of California Santa Barbara,1999. [2] Bernero S,Fiedler H E. Simultaneous PIV and LIF experiments on a round jet in counterflow . Proc 1st Int Symp on Turbulence and Shear Flow Phenomena .CA,Santa Barbara, US:Univ of California Santa Barbara,1999. [3] Bernero S,Fiedler H E. Experimental investigations of a jet in counterflow . 7th European Turbulence Conference(ETGF) Saint Jean Cap Ferrat . France, European Mechanics Society, 1998.35~38. [4] Ross C,Lourenceo L,Krothapalli A. PIV measurements in a shock-containing supersonic flow . AIAA paper 94-0047,1994.
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