Skip to main content
Log in

Characteristics of spherical shock wave and circular pulse jet generated by discharge of propagating shock wave at open end of tube

  • Published:
Journal of Thermal Science Aims and scope Submit manuscript

Abstract

When the shock wave propagating in the straight circular tube reaches at the open end, the impulsive wave is generated by the emission of a shock wave from an open end, and unsteady pulse jet is formed near the open end behind the impulsive wave under the specific condition. The pulse jet transits to spherical shock wave with the increase in the strength of shock wave. The strength is dependent on the Mach number of shock wave, which attenuates by propagation distance from the open end. In this study, the mechanism of generating the unsteady pulse jet, the characteristics of the pressure distribution in the flow field and the emission of shock wave from straight circular tube which has the infinite flange at open end are analyzed numerically by the TVD method. Strength of spherical shock wave, relation of shock wave Mach number, distance decay of spherical shock wave and directional characteristics are clarified.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. Croes, N. The Principle of the Pressure Wave Machine Used for Charging Diesel Engines. Proc. 11th Int. Symp. Shock Tubes and Waves. Seattle, 1977. 36–55

  2. Eidelman, S, et al. A Propulsion Device Driven by Reflected Shock Waves. Shock Waves, 1992, II: 1283–1288

    Google Scholar 

  3. Ruppert, K A, et al. The Effect of Multiple Pressure Pulses Cleaning of Filter Bags. Ger. Chem. Eng., 1984, 7: 345–349

    Google Scholar 

  4. Kuhl, A L, et al. Fluid Mechanics of a Planar Exothermic Jet. JSME ICFE-97. Tokyo, 1997, 955–959

  5. Abe, A, Takayama, K. Numerical Simulation and Density Measurement of a Shock Wave Discharged from the Open End of a Tube. JSME Int. J., 1990, 33(2): 216–223

    Google Scholar 

  6. Ishii, R, et al. Experimental and Numerical Analysis of Circular Pulse Jets. J. Fluid Mech., 1990, 392: 129–153

    Article  ADS  Google Scholar 

  7. Endo, M, Iwamoto, J. A Study of Pulsatile Jet Discharged from Pipe End. J. of Visualization, 1999, 1(3): 261–269

    Article  Google Scholar 

  8. Setoguchi, T, et al. Discharge of a Weak Shock Wave from an Open End of a Tube. Nati. Symp. Shock Wave Phenomena. Sagamihara, 1989, 31–40

  9. Yee, H C. NASA Tech. Mem., 1987, 89464

  10. Sod, G A. A Numerical Study of a Converging Cylindrical Shock. J. Fluid Mech., 1977, 83(Part 4): 785–794

    Article  MATH  ADS  Google Scholar 

  11. Adamson, Jr T C, Nicholls, J A. On the Structure of Jets from Highly Underexpanded Nozzles into Still Air. J. Aero/Space Sci., 1959, 16–24

  12. Ashkenas, H, Sherman, F S. The Structure and Utilization of Supersonic Free Jets in Low Density Wind Tunnels. Proc. 4th Int. Symp. Rarefied Gas Dyn., 1966, 2: 84–105

    ADS  Google Scholar 

  13. Addy, A L. Effects of Axisymmetric Sonic Nozzle Geometry on Mach Disk Characteristics. AIAA J., 1981, 19(1): 121–122

    Article  ADS  Google Scholar 

  14. Aizik, F, et al. General Attenuation Laws for Spherical Shock Waves in Pure and Dusty Gases. AIAA J., 2000, 39(5): 969–971

    ADS  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Irie, T., Yasunobu, T., Kashimura, H. et al. Characteristics of spherical shock wave and circular pulse jet generated by discharge of propagating shock wave at open end of tube. J. of Therm. Sci. 12, 245–249 (2003). https://doi.org/10.1007/s11630-003-0076-y

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11630-003-0076-y

Keywords

Navigation