Preliminary Experimental Study on Pressure Loss Coefficients of Exhaust Manifold Junction

• Main Authors: Xiao-lu Lu, Kun Zhang, Wen-hui Wang, Shao-ming Wang, Kang-yao Deng
• Format: Article
• Language: English
• Published: Hindawi Limited 2014-01-01
• Series: International Journal of Rotating Machinery
• Online Access: http://dx.doi.org/10.1155/2014/316498

The flow characteristic of exhaust system has an important impact on inlet boundary of the turbine. In this paper, high speed flow in a diesel exhaust manifold junction was tested and simulated. The pressure loss coefficient of the junction flow was analyzed. The steady experimental results indicated that both of static pressure loss coefficients L13 and L23 first increased and then decreased with the increase of mass flow ratio of lateral branch and public manifold. The total pressure loss coefficient K13 always increased with the increase of mass flow ratio of junctions 1 and 3. The total pressure loss coefficient K23 first increased and then decreased with the increase of mass flow ratio of junctions 2 and 3. These pressure loss coefficients of the exhaust pipe junctions can be used in exhaust flow and turbine inlet boundary conditions analysis. In addition, simulating calculation was conducted to analyze the effect of branch angle on total pressure loss coefficient. According to the calculation results, total pressure loss coefficient was almost the same at low mass flow rate of branch manifold 1 but increased with lateral branch angle at high mass flow rate of branch manifold 1.