performance experimental data of 14 units of domestic axial flow fans and compressors were collected. Two kinds of basic attributes were presented to describe aerodynamic performances of fan and compressor based on analysis and identification of shape structure of off-design characteristic curves of high mass flow fan and high pressure ratio compressor. In an attempt to build a number of non-dimensional physical parameters
the quantitative correlative relationship between shift degree under variable speed and operating range under constant speed of characteristics of fans and compressors was explored in the statistical level. The results show that offset degree of non-design rotating speed characteristic lines and operating range of effective mass flow of fans are greater than that of high pressure ratio compressors
and the relative pressure ratio
relative mass flow
relative mass flow-speed ratio and relative work-speed ratio on peak efficiency line of fans and compressors exhibit obvious statistical regularity. The uniform correlative analysis of performance experimental data can be conducted by means of some empirical mathematical models presented.
Discussion on several problems of axial flow fan/compressor aerodynamic performance experiment
Impact of Reynolds number on unsteady flow in axial flow compressor rotor
Numerical study on water film formation on aerodynamic effect of axial flow fan
Accuracy analysis of unsteady numerical simulation methods for axial flow compressor
Effects of oxide layer non-uniform growth on thermal barrier coating stress distribution
Related Author
XIANG Hong-hui
GE Ning
WEN Zhen-rong
AN Jinhuaiyuan
WU Yanhui
CHEN Zhiyang
WU Feng
HOU Shengwen
Related Institution
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
北京航空航天大学 能源与动力工程学院
先进航空发动机协同创新中心
Key Laboratory on Aero-engine Altitude Simulation Technology, China Gas Turbine Establishment, Aviation Industry Corporation of China, Jiangyou Sichuan
College of Power and Energy Engineering,Harbin Engineering University