为缓解环境污染,提高终端用能效率,综合能源系统(integrated energy system,IES)已成为我国能源结构调整的重要方向。在IES框架下,传统以电力系统为对象的潮流计算方法将难以满足对互相耦合的能量流分析的需求。提出了一种适用于含电、...为缓解环境污染,提高终端用能效率,综合能源系统(integrated energy system,IES)已成为我国能源结构调整的重要方向。在IES框架下,传统以电力系统为对象的潮流计算方法将难以满足对互相耦合的能量流分析的需求。提出了一种适用于含电、热、气的IES的扩展Newton-Raphson多能流计算方法。首先,分别建立了IES中电力、热力和天然气网络的数学模型;针对现有方法对含压缩机的天然气网络建模的繁冗性问题,计及不同的控制方式,提出了改进的实用化处理方法;在此基础上,进一步构建了IES多能流计算模型,考虑IES中电力系统并网和孤岛2种运行方式,推导并得出了反映多能源耦合关系的雅可比矩阵。算例验证了该方法在不同运行场景下对多能流进行计算和互动特性分析的有效性。展开更多
NASA rotor 37 was used as a ’blind’ test case for turbomachinery CFD by the Turbimachinery Com-mittee of the IGTI. The rotor is a transonic compressor with a tip speed of 454 m/s (15OO ft/s) anda relatively high pre...NASA rotor 37 was used as a ’blind’ test case for turbomachinery CFD by the Turbimachinery Com-mittee of the IGTI. The rotor is a transonic compressor with a tip speed of 454 m/s (15OO ft/s) anda relatively high pressure ratio of 2.1. It was tested in isolation with a circumferentially uniform inletflow so that the flow through it should be steady apart from any effects of passage to passage geometry variation and mechanical vibration. As such it represents the simplest possible type of test forthree-dimensional turbomachinery flow solvers. However, the rotor still presents a real challenge to3D viscous flow solvers because the shock wave-boundary layer interaction is strong and the effects ofviscosity are dominant in determining the flow deviation and hence the pressure ratio. Eleven ’blind’solutions were submitted and in addition a ’non-blind’ solution was used to prepare for the exercise-This paper reviews the fiow in the test case and the comparisons of the CFD solutions with the testdata. Lessons for both the Flow Physics in transonic has and for the application of CFD to suchmachines are pointed out.展开更多
文摘为缓解环境污染,提高终端用能效率,综合能源系统(integrated energy system,IES)已成为我国能源结构调整的重要方向。在IES框架下,传统以电力系统为对象的潮流计算方法将难以满足对互相耦合的能量流分析的需求。提出了一种适用于含电、热、气的IES的扩展Newton-Raphson多能流计算方法。首先,分别建立了IES中电力、热力和天然气网络的数学模型;针对现有方法对含压缩机的天然气网络建模的繁冗性问题,计及不同的控制方式,提出了改进的实用化处理方法;在此基础上,进一步构建了IES多能流计算模型,考虑IES中电力系统并网和孤岛2种运行方式,推导并得出了反映多能源耦合关系的雅可比矩阵。算例验证了该方法在不同运行场景下对多能流进行计算和互动特性分析的有效性。
文摘NASA rotor 37 was used as a ’blind’ test case for turbomachinery CFD by the Turbimachinery Com-mittee of the IGTI. The rotor is a transonic compressor with a tip speed of 454 m/s (15OO ft/s) anda relatively high pressure ratio of 2.1. It was tested in isolation with a circumferentially uniform inletflow so that the flow through it should be steady apart from any effects of passage to passage geometry variation and mechanical vibration. As such it represents the simplest possible type of test forthree-dimensional turbomachinery flow solvers. However, the rotor still presents a real challenge to3D viscous flow solvers because the shock wave-boundary layer interaction is strong and the effects ofviscosity are dominant in determining the flow deviation and hence the pressure ratio. Eleven ’blind’solutions were submitted and in addition a ’non-blind’ solution was used to prepare for the exercise-This paper reviews the fiow in the test case and the comparisons of the CFD solutions with the testdata. Lessons for both the Flow Physics in transonic has and for the application of CFD to suchmachines are pointed out.
