Starting from the typical dynamic characteristics of the complete rotating stall process of low-speed axial compressor
such as catastrophe and hysteresis
by comparing and analyzing the topological properties
the rotating stall and cusp catastrophic model of catastrophe theory were proved similar in spatial topology; then
based on the topological invariance theorem through developing the effective topological mapping method
the topological mapping relationship of the catastrophe point set between the rotating stall and the cusp catastrophic model was established. The applied effect of the model in two low-speed axial compressors showed that cusp catastrophic model can qualitatively describe the catastrophe
hysteresis and bifurcation of the complete rotating stall process of low-speed compressor with the characteristic of “abrupt stall” under different speed conditions; through the mapping method developed
the stall points and recovery points obtained by experiment can be entirely mapped to the model line
which means the cusp catastrophic model can accurately describe the instability boundary of rotating stall.
Effects of rotating disturbance on aerodynamics stability of axial-flow compressor
Numerical simulation on stall margin improvement of transonic compressor by a trapped vortex casing treatment
Experiment on axial-compressor stability enhancement by blade tip injection
Experiment on single axial compressor of characteristic of rotating stall
Identification of stall characteristics of axial flow compressor
Related Author
MAO Zhi-ming
HU Jun
ZHANG Huan
YAN Wei
WANG Zhuo-qi
LU Li-peng
YUAN Wei
SONG Xi-zhen
Related Institution
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
Research Institute of Unmanned Aerial Vehicle, Beijing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
School of Power and Energy,Northwestern Polytechnical University
Science and Technology Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University