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Payganeh, Gh., Hadidi, A., Hallaji, M., Garjasi, N.. (1390). The numerical simulation of compressible flow in a Shubin nozzle using schemes of Bean-Warming and flux vector splitting. فناوری آموزش, 1(2), 111-118. doi: 10.22061/jcarme.2012.31
Gh. Payganeh; A. Hadidi; M. Hallaji; N. Garjasi. "The numerical simulation of compressible flow in a Shubin nozzle using schemes of Bean-Warming and flux vector splitting". فناوری آموزش, 1, 2, 1390, 111-118. doi: 10.22061/jcarme.2012.31
Payganeh, Gh., Hadidi, A., Hallaji, M., Garjasi, N.. (1390). 'The numerical simulation of compressible flow in a Shubin nozzle using schemes of Bean-Warming and flux vector splitting', فناوری آموزش, 1(2), pp. 111-118. doi: 10.22061/jcarme.2012.31
Payganeh, Gh., Hadidi, A., Hallaji, M., Garjasi, N.. The numerical simulation of compressible flow in a Shubin nozzle using schemes of Bean-Warming and flux vector splitting. فناوری آموزش, 1390; 1(2): 111-118. doi: 10.22061/jcarme.2012.31

The numerical simulation of compressible flow in a Shubin nozzle using schemes of Bean-Warming and flux vector splitting

Journal of Computational & Applied Research in Mechanical Engineering (JCARME)
مقاله 5، دوره 1، شماره 2، شهریور 2012، صفحه 111-118    اصل مقاله (690.13 K)
نوع مقاله: Research Paper
شناسه دیجیتال (DOI): 10.22061/jcarme.2012.31
نویسندگان
Gh. Payganeh1؛ A. Hadidi* 2؛ M. Hallaji2؛ N. Garjasi2
1Department of Mechanical Engineering, Shahid Rajaee Teacher Training University, Lavizan, Tehran, Iran
2Department of Mechanical Engineering, Tarbiat Modares University, Tehran, Iran
تاریخ دریافت: 17 مرداد 1390،  تاریخ بازنگری: 12 آبان 1390،  تاریخ پذیرش: 17 آبان 1390 
چکیده
Over the last ten years, robustness of schemes has raised an increasing interest among the CFD community. The objective of this article is to solve the quasi-one-dimensional compressible flow inside a “Shubin nozzle” and to investigate Bean-Warming and flux vector splitting methods for numerical solution of compressible flows. Two different conditions have been considered: first, there is a supersonic flow in the entry and a supersonic flow in the outlet, without any shock in the nozzle. Second, there is a supersonic flow in the inlet and a subsonic flow in the outlet of the nozzle and a shock occur inside the nozzle. The results show that the run time of the flux vector splitting scheme is more than the Bean-Warming scheme, and, the flux vector splitting scheme is more accurate than the Bean-Warming scheme. However the flux vector splitting scheme is more complicated. 
کلیدواژه‌ها
Compressible flow؛ Shubin nozzle؛ Bean-Warming scheme؛ Flux vector splitting scheme؛ Euler equation
مراجع

[1] B. VanLeer, "Flux-vector splitting for the Euler equations", Eighth International Conferenceon Numerical Methods in Fluid Dynamics, Germany, (1982).

[2] R. Bean and R. Warming, "An implicit finite-difference algorithm for hyperbolic systems in conservation law form", Journal of ComputationalPhysics, Vol. 22, pp. 87-110,(1976).

[3] R. Bean and R. Warming, "An implicit factored scheme for the compressible Navier-Stokes equations", American Instof Aeronauticsand Astronautics, Vol. 16, pp. 393-402, (1977).

[4] G. May and A. Jameson, "A spectral difference method for the Euler and Navier-Stokes equations on unstructured meshes", AIAA 44th Aerospace Science Meeting and Exhibit, (2006).

[5] H. Bucker, B. Pollul and A. Rasch, "On CFL evolution strategies for implicit upwind methods in linearized Euler equations", International Journal for Numerical Methods in Fluid, Vol. 59, pp1-18, (2009).

[6] R. Warming and R. B., "Upwind second-order difference schemes and applications in aerodynamic flows", American Inst of Aeronautics and Astronautics,Vol. 14, pp 1241-1249, (1976).

[7] J. Qiu, "Development and comparison of numerical fluxes for LWDG methods", Numerical Mathematics, Theory, Methods and Application, Vol. 1, pp. 1-32, (2008).

[8] J. Steger, "finite difference simulation of flow about arbitrary geometries with application to airfoils", American Inst of Aeronautics and Astronautics, Vol. 16, pp. 679-686, (1978).

[9] D. W. Zingg, S. De Rango, M. Nemec and T. H. Pulliam, "Comparison of several spatial discretizations for the Navier-Stokes Equations", Journal of computational Physics, Vol. 160, pp683-704, (2000).

[10] T. H. Pulliam, "Early development of implicit methods for Computational Fluid Dynamics at NASA Ames", Computers and fluid, Vol. 38, pp. 491-495, (2009).

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