Solution of the turbocompressor boundary condition for one-dimensional gas-dynamic codes
نویسندگان
چکیده
Nowadays, turbocharged engines are widely used in cars and trucks. Gas dynamic codes are an important tool in design and optimization of this type of engine. These codes solve one-dimensional governing equations in ducts for compressible, unsteady and non-homoentropic flow. The ducts are generally solved using finite difference schemes, the volumes are solved by means of filling and emptying models and the connections represents the boundary conditions of the ducts. One important boundary condition are the compressor which join two duct. In this junction an increment of momentum and energy is undergo but depending of the flow direction the behavior is different. The solution involves a complex equation system that can be solved iteratively. Different root-finding algorithms like Bisection method or Newton-Raphson method will be compared.
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ورودعنوان ژورنال:
- Mathematical and Computer Modelling
دوره 52 شماره
صفحات -
تاریخ انتشار 2010