Abstract
That shock passes through a gas particle suspension called as particle cloud layer, then, diffracts over a wedge were numerically investigated in this paper. The wedge is posed along the lower duct wall. Two-fluid model was used to describe the dilute, two-phase flow. Fully Reynolds averaged Navier-Stokes equations were solved by upwind TVD scheme for gas phase. Eulerian equations were solved by NND scheme for dispersed phase. The phase interaction equations, involving drag force and heat transfer between the gas and particles, were solved by 2nd Runge-Kutta approach. Also, several parameters, i. e. droplet diameter, particle cloud layer position, moving shock Mach number and wedge height, were tested to show their effects to the two-phase flow field. The distributions of contours for gas pressure and density of dispersed phase were obtained at different time intervals. The results show the evolution of the shock and demonstrate the effects of key parameter to the flow field of the two-phase flow. Such a two-phase flow field is much more complicated than that of particle free gas flow.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Jr. Peddieson: Gas particle flow past bodies with attached shock waves. AIAA J. 13(7), 939 (1975)
J.M. Pascaud, J. Brossard: Predictive method of pressure venting for dust explosion in large vessels. J. of Combustion Science and Technology 138, 159 (1998)
E. Outa, T. Tajima, H. Morii: Experiments and analysis of shock waves propagating through a gas-particle mixture. Bulletin JSME 19, 348 (1976)
O. Igra, G. Ben-Dor: Dusty shock waves. Applied Mechanics Rev. 41(1), 397 (1988)
Richard Saurel, Eric Daniel, Jean Claude Loraud: Two phase flows: Second-order schemes and boundary condition. AIAA J. 32(6), 1214 (1994)
R. Ishii, Y. Umeda, M. Yuhi: Numerical analysis of gas-particle two phase flows. J of Fluid Mechanics 203, 475 (1989)
H.C. Yee: Upwind and symmetric shock-capturing schemes. NASA 89464 (1987)
H.X. Zhang, Z.W. Li: Numerical simulation on hypersonic laminar wahe flow. ACTA Mechanica Sinica, 24(4), 389 (1992)
S.L. Xu, P.T. Yue, Z.Y. Han et al.: Numerical simulation of atomized fuels transversely injected into a supersonic flow. ACTA Aerodynamica Sinica, 18(1), 39 (2000) (in Chinese)
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2005 Tsinghua University Press and Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Xu, S.L., Han, S., Yue, P.T., Yang, J.M., Archer, R.D. (2005). Numerical investigation on shock passing through a gas particle suspension and diffracting over a wedge in a duct. In: Jiang, Z. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-27009-6_82
Download citation
DOI: https://doi.org/10.1007/978-3-540-27009-6_82
Published:
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-22497-6
Online ISBN: 978-3-540-27009-6
eBook Packages: Physics and AstronomyPhysics and Astronomy (R0)