机械
Chord(对等)
入口
空气动力学
涡轮机
前沿
井式水轮机
后缘
浪涌
物理
涡轮叶片
流量(数学)
工程类
航空航天工程
气象学
机械工程
计算机科学
分布式计算
作者
Yixiong Liu,Ce Yang,Dengfeng Yang,Rui Zhang
出处
期刊:International journal of turbo & jet-engines
[De Gruyter]
日期:2015-04-17
卷期号:33 (1)
标识
DOI:10.1515/tjj-2015-0009
摘要
Abstract The aerodynamic performance, detailed unsteady flow and time-based excitations acting on blade surfaces of a radial flow turbine have been investigated with pulsation flow condition. The results show that the turbine instantaneous performance under pulsation flow condition deviates from the quasi-steady value significantly and forms obvious hysteretic loops around the quasi-steady conditions. The detailed analysis of unsteady flow shows that the characteristic of pulsation flow field in radial turbine is highly influenced by the pulsation inlet condition. The blade torque, power and loading fluctuate with the inlet pulsation wave in a pulse period. For the blade excitations, the maximum and the minimum blade excitations conform to the wave crest and wave trough of the inlet pulsation, respectively, in time-based scale. And toward blade chord direction, the maximum loading distributes along the blade leading edge until 20% chord position and decreases from the leading to trailing edge.
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