Experimental Study of the Vibration Phenomenon of Compressor Rotor Blade Induced by Inlet Probe Support
Authors:
- 6 April 2021
- journal article
- research article
- Published by Springer Nature in Journal of Thermal Science
- Vol. 30 (5) , 1674-1683
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Effects of probe support on the stall characteristics of a low-speed axial compressorJournal of Thermal Science, 2016
- Effects of probe support on the flow field of a low-speed axial compressorJournal of Thermal Science, 2014
- Investigation of the Effects of Airfoil-probes on the Aerodynamic Performance of an Axial CompressorChinese Journal of Aeronautics, 2012
- Unsteady Flow in a Turbocharger Centrifugal Compressor: Three-Dimensional Computational Fluid Dynamics Simulation and Numerical and Experimental Analysis of Impeller Blade VibrationJournal of Turbomachinery, 2005
- Time-Linearized Navier-Stokes Analysis of Flutter in Multistage Turbomachines2005
- Time-Resolved Vane-Rotor Interaction in a High-Pressure Turbine StageJournal of Turbomachinery, 2003
- Considerations for Using 3D Pneumatic Probes in High Speed Axial Compressors2002
- Aerodynamic Effects on Blade Vibratory Stress VariationsJournal of Propulsion and Power, 1999
- Flutter and Resonant Vibration Characteristics of Engine BladesJournal of Engineering for Gas Turbines and Power, 1997
- Optimization applications for aircraft engine design and manufactureAdvances in Engineering Software, 1993