Modified Pressure Loss Model for T-junctions of Engine Exhaust Manifold

The T-junction model of engine exhaust manifolds significantly influences the simulation precision of the pressure wave and mass flow rate in the intake and exhaust manifolds of diesel engines. Current studies have focused on constant pressure models, constant static pressure models and pressure los...

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Veröffentlicht in:Chinese journal of mechanical engineering 2014-11, Vol.27 (6), p.1232-1239
Hauptverfasser: Wang, Wenhui, Lu, Xiaolu, Cui, Yi, Deng, Kangyao
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creator Wang, Wenhui
Lu, Xiaolu
Cui, Yi
Deng, Kangyao
description The T-junction model of engine exhaust manifolds significantly influences the simulation precision of the pressure wave and mass flow rate in the intake and exhaust manifolds of diesel engines. Current studies have focused on constant pressure models, constant static pressure models and pressure loss models. However, low model precision is a common disadvantage when simulating engine exhaust manifolds, particularly for turbocharged systems. To study the performance of junction flow, a cold wind tunnel experiment with high velocities at the junction of a diesel exhaust manifold is performed, and the variation in the pressure loss in the T-junction under different flow conditions is obtained. Despite the trend of the calculated total pressure loss coefficient, which is obtained by using the original pressure loss model and is the same as that obtained from the experimental results, large differences exist between the calculated and experimental values. Furthermore, the deviation becomes larger as the flow velocity increases. By improving the Vazsonyi formula considering the flow velocity and introducing the distribution function, a modified pressure loss model is established, which is suitable for a higher velocity range. Then, the new model is adopted to solve one-dimensional, unsteady flow in a D6114 turbocharged diesel engine. The calculated values are compared with the measured data, and the result shows that the simulation accuracy of the pressure wave before the turbine is improved by 4.3% with the modified pressure loss model because gas compressibility is considered when the flow velocities are high. The research results provide valuable information for further junction flow research, particularly the correction of the boundary condition in one-dimensional simulation models.
doi_str_mv 10.3901/CJME.2014.0904.143
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Current studies have focused on constant pressure models, constant static pressure models and pressure loss models. However, low model precision is a common disadvantage when simulating engine exhaust manifolds, particularly for turbocharged systems. To study the performance of junction flow, a cold wind tunnel experiment with high velocities at the junction of a diesel exhaust manifold is performed, and the variation in the pressure loss in the T-junction under different flow conditions is obtained. Despite the trend of the calculated total pressure loss coefficient, which is obtained by using the original pressure loss model and is the same as that obtained from the experimental results, large differences exist between the calculated and experimental values. Furthermore, the deviation becomes larger as the flow velocity increases. By improving the Vazsonyi formula considering the flow velocity and introducing the distribution function, a modified pressure loss model is established, which is suitable for a higher velocity range. Then, the new model is adopted to solve one-dimensional, unsteady flow in a D6114 turbocharged diesel engine. The calculated values are compared with the measured data, and the result shows that the simulation accuracy of the pressure wave before the turbine is improved by 4.3% with the modified pressure loss model because gas compressibility is considered when the flow velocities are high. The research results provide valuable information for further junction flow research, particularly the correction of the boundary condition in one-dimensional simulation models.</description><edition>English ed.</edition><identifier>ISSN: 1000-9345</identifier><identifier>EISSN: 2192-8258</identifier><identifier>DOI: 10.3901/CJME.2014.0904.143</identifier><language>eng</language><publisher>Beijing: Chinese Mechanical Engineering Society</publisher><subject>Boundary conditions ; Cold flow ; Cold junctions ; Compressibility ; Computer simulation ; Constants ; Diesel engines ; Distribution functions ; Elastic waves ; Electrical Machines and Networks ; Electronics and Microelectronics ; Engineering ; Engineering Thermodynamics ; Exhaust ; Exhaust systems ; Flow velocity ; Heat and Mass Transfer ; Instrumentation ; Machines ; Manifolds ; Manufacturing ; Mass flow rate ; Mathematical analysis ; Mathematical models ; Mechanical Engineering ; Power Electronics ; Pressure loss ; Processes ; Simulation ; Static pressure ; Stress concentration ; Superchargers ; Theoretical and Applied Mechanics ; Turbines ; Unsteady flow ; Wind tunnel testing ; Wind tunnels ; 丁字路口 ; 修改 ; 压力损失系数 ; 压力波 ; 损耗模型 ; 排气歧管 ; 柴油发动机 ; 涡轮增压系统</subject><ispartof>Chinese journal of mechanical engineering, 2014-11, Vol.27 (6), p.1232-1239</ispartof><rights>Chinese Mechanical Engineering Society and Springer-Verlag Berlin Heidelberg 2014</rights><rights>Chinese Journal of Mechanical Engineering is a copyright of Springer, (2014). 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Eng</addtitle><addtitle>Chinese Journal of Mechanical Engineering</addtitle><description>The T-junction model of engine exhaust manifolds significantly influences the simulation precision of the pressure wave and mass flow rate in the intake and exhaust manifolds of diesel engines. Current studies have focused on constant pressure models, constant static pressure models and pressure loss models. However, low model precision is a common disadvantage when simulating engine exhaust manifolds, particularly for turbocharged systems. To study the performance of junction flow, a cold wind tunnel experiment with high velocities at the junction of a diesel exhaust manifold is performed, and the variation in the pressure loss in the T-junction under different flow conditions is obtained. Despite the trend of the calculated total pressure loss coefficient, which is obtained by using the original pressure loss model and is the same as that obtained from the experimental results, large differences exist between the calculated and experimental values. Furthermore, the deviation becomes larger as the flow velocity increases. By improving the Vazsonyi formula considering the flow velocity and introducing the distribution function, a modified pressure loss model is established, which is suitable for a higher velocity range. Then, the new model is adopted to solve one-dimensional, unsteady flow in a D6114 turbocharged diesel engine. The calculated values are compared with the measured data, and the result shows that the simulation accuracy of the pressure wave before the turbine is improved by 4.3% with the modified pressure loss model because gas compressibility is considered when the flow velocities are high. 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J. Mech. Eng</stitle><addtitle>Chinese Journal of Mechanical Engineering</addtitle><date>2014-11-01</date><risdate>2014</risdate><volume>27</volume><issue>6</issue><spage>1232</spage><epage>1239</epage><pages>1232-1239</pages><issn>1000-9345</issn><eissn>2192-8258</eissn><abstract>The T-junction model of engine exhaust manifolds significantly influences the simulation precision of the pressure wave and mass flow rate in the intake and exhaust manifolds of diesel engines. Current studies have focused on constant pressure models, constant static pressure models and pressure loss models. However, low model precision is a common disadvantage when simulating engine exhaust manifolds, particularly for turbocharged systems. To study the performance of junction flow, a cold wind tunnel experiment with high velocities at the junction of a diesel exhaust manifold is performed, and the variation in the pressure loss in the T-junction under different flow conditions is obtained. Despite the trend of the calculated total pressure loss coefficient, which is obtained by using the original pressure loss model and is the same as that obtained from the experimental results, large differences exist between the calculated and experimental values. Furthermore, the deviation becomes larger as the flow velocity increases. By improving the Vazsonyi formula considering the flow velocity and introducing the distribution function, a modified pressure loss model is established, which is suitable for a higher velocity range. Then, the new model is adopted to solve one-dimensional, unsteady flow in a D6114 turbocharged diesel engine. The calculated values are compared with the measured data, and the result shows that the simulation accuracy of the pressure wave before the turbine is improved by 4.3% with the modified pressure loss model because gas compressibility is considered when the flow velocities are high. The research results provide valuable information for further junction flow research, particularly the correction of the boundary condition in one-dimensional simulation models.</abstract><cop>Beijing</cop><pub>Chinese Mechanical Engineering Society</pub><doi>10.3901/CJME.2014.0904.143</doi><tpages>8</tpages><edition>English ed.</edition><oa>free_for_read</oa></addata></record>
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ispartof Chinese journal of mechanical engineering, 2014-11, Vol.27 (6), p.1232-1239
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source Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals; Alma/SFX Local Collection
subjects Boundary conditions
Cold flow
Cold junctions
Compressibility
Computer simulation
Constants
Diesel engines
Distribution functions
Elastic waves
Electrical Machines and Networks
Electronics and Microelectronics
Engineering
Engineering Thermodynamics
Exhaust
Exhaust systems
Flow velocity
Heat and Mass Transfer
Instrumentation
Machines
Manifolds
Manufacturing
Mass flow rate
Mathematical analysis
Mathematical models
Mechanical Engineering
Power Electronics
Pressure loss
Processes
Simulation
Static pressure
Stress concentration
Superchargers
Theoretical and Applied Mechanics
Turbines
Unsteady flow
Wind tunnel testing
Wind tunnels
丁字路口
修改
压力损失系数
压力波
损耗模型
排气歧管
柴油发动机
涡轮增压系统
title Modified Pressure Loss Model for T-junctions of Engine Exhaust Manifold
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