The numerical simulation of compressible flow in a Shubin nozzle using schemes of Bean-Warming and flux vector splitting
نویسندگان
1 Department of Mechanical Engineering, Shahid Rajaee Teacher Training University, Lavizan, Tehran, Iran
2 Department of Mechanical Engineering, Tarbiat Modares University, Tehran, Iran
3 Department of Mechanical Engineering, Tarbiat Modares University, Tehran, Iran
4 Department of Mechanical Engineering, Tarbiat Modares University, Tehran, Iran
doi
10.22061/jcarme.2012.31چکیده
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.
