Vibration Analysis of Blade Under Multiple Composite Unsteady Excitations
In order to understand the effects of the unsteady aerodynamic excitations in complex flow field on blades, on the basis of the data obtained from the single-stage axial flow compressor, three kinds of exciting forms in the compressor had been studied, including the correlation between excitations...
Main Authors: | Licheng FANG, Shunming LI, Sai MA, Jiyong LI |
---|---|
Format: | Article |
Language: | English |
Published: |
IFSA Publishing, S.L.
2014-01-01
|
Series: | Sensors & Transducers |
Subjects: | |
Online Access: | http://www.sensorsportal.com/HTML/DIGEST/january_2014/Vol_162/P_1770.pdf |
Similar Items
-
A Study on the Stall Detection of an Axial Compressor through Pressure Analysis
by: Haoying Chen, et al.
Published: (2017-07-01) -
Analysis of the Effects of Inlet Distortion on Stall Cell Formation in a Transonic Compressor Using CREATE-AV Kestrel
by: Unrau, Mikkel Andreas
Published: (2018) -
Excitation System Technologies for Wound-Field Synchronous Machines: Survey of Solutions and Evolving Trends
by: Jonas Kristiansen Noland, et al.
Published: (2019-01-01) -
High Fidelity Time Accurate CFD Analysis of a Multi-stage Turbofan at Various Operating Points in Distorted Inflow
by: Weston, David Bruce
Published: (2014) -
Numerical simulation of dynamic stall phenomena in axial flow compressor blade rows
by: Rivera-Cedeno, Carlos J.
Published: (2006)