hub region initiated disturbance by experimental investigations in a transonic compressor. In term of physical mechanisms
partial surge was much similar to an oscillation in a Helmholtz system. By Duct-Compressor-Plenum model
the Helmholtz frequency of the system was estimated
which was very close to the frequency of partial surge. To further verify this link between the frequency of partial surge and the Helmholtz frequency
experimental investigations were carried out with variation of specific parameters of the Helmholtz system. The results present that the frequency of partial surge varies with the Helmholtz frequency of the system. And the values of both frequency are very close. Therefore
the frequency of partial surge is determined by the Helmholtz frequency of the system.
Experiment on the instability process in a one-stage transonic axial compressor
Research on transient load for transonic compressor based on dynamic boundaries
Improved viscous inverse design method for three-dimensional turbomachinery blades
Numerical simulation on blade tip unsteady flow in transonic compressor rotor
Related Author
LI Qiu-shi
LI Zhi-ping
SUN Tai-lu
PAN Tian-yu
HE Lei
GUO Qiannan
YANG Caiqiong
ZHANG Weiya
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Sichuan Gas Turbine Establishment,Aero Engine Corporation of China