NUMERICAL SOLUTION OF COMPRESSIBLE FLOW EQUATIONS INSIDE AN EJECTOR

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OMIDKHAH M.R.; NAVID FAMILI M.H.; JALILI KESHTIBAN E.

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Paper Information

Journal: Nashrieh Shimi va Mohandesi Shimi Iran Year:2002 | Volume:21 | Issue:1-2 Page(s): 11-21

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Title

NUMERICAL SOLUTION OF COMPRESSIBLE FLOW EQUATIONS INSIDE AN EJECTOR

Author(s)

OMIDKHAH M.R. | NAVID FAMILI M.H. | JALILI KESHTIBAN E. | Issue Writer Certificate

Keywords

EJECTORQ4

COMPRESSIBLE FLOWQ4

FINITE VOLUMEQ4

SIMPLEC METHODQ4

SHOCK BEHAVIOURQ4

INSTABILITYQ4

VISCOUS FLUIDQ4

INVISCID FLUIDQ4

Abstract

EJECTOR is important equipment in the chemical industry. It is mainly used for vacuuming and mixing of flows. In the present work a computer modeling of the flow inside an EJECTOR is used to give a better understanding of the principle of the operation of an EJECTOR. Since the fluid inside an EJECTOR passes through sub sonic, sonic and super sonic regimens, the pressure field is used as the controlling variable and the density is found through the constitutive equations. The control volume method with a co-location grid, attached to the boundary is used to discretize the domain. The overall solution is obtained by the SIMPLE method and to dissociate the pressure and the velocity grid Rhie-Chow interpolation method is employed A central difference approximation method is used to approximate the density on the element borders and the upwind approximation is used to correct the density correction factors. Both upwind, quick and minimum gradient methods were used to approximate the momentum variables on the control volumes. The resultant matrices are solved with the tri-diagonal method the accuracy of the model is checked by simulating a flow regimen in a converging-diverging nozzle, and comparing the results with the available experimental data. The results show that for an INVISCID FLUID the first order approximation produce as accurate results as the higher order approximations while it has a better stability. However, for the viscous fluid the second order approximation produces a better understanding of the physics of the problem. The solution also shows that the flow field inside an EJECTOR is a complex one and the shock wave has a great influence on the pressure field especially close to the walls. The upper convective quick method did not converg well in the shock calculations while the slowest descent method had a very stable behavior in the analysis of the shock behavior.

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APA: Copy

OMIDKHAH, M.R., NAVID FAMILI, M.H., & JALILI KESHTIBAN, E.. (2002). NUMERICAL SOLUTION OF COMPRESSIBLE FLOW EQUATIONS INSIDE AN EJECTOR. NASHRIEH SHIMI VA MOHANDESI SHIMI IRAN (PERSIAN), 21(1-2), 11-21. SID. https://sid.ir/paper/26167/en

Vancouver: Copy

OMIDKHAH M.R., NAVID FAMILI M.H., JALILI KESHTIBAN E.. NUMERICAL SOLUTION OF COMPRESSIBLE FLOW EQUATIONS INSIDE AN EJECTOR. NASHRIEH SHIMI VA MOHANDESI SHIMI IRAN (PERSIAN)[Internet]. 2002;21(1-2):11-21. Available from: https://sid.ir/paper/26167/en

IEEE: Copy

M.R. OMIDKHAH, M.H. NAVID FAMILI, and E. JALILI KESHTIBAN, “NUMERICAL SOLUTION OF COMPRESSIBLE FLOW EQUATIONS INSIDE AN EJECTOR,” NASHRIEH SHIMI VA MOHANDESI SHIMI IRAN (PERSIAN), vol. 21, no. 1-2, pp. 11–21, 2002, [Online]. Available: https://sid.ir/paper/26167/en

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