Investigation of Flow Instability Mechanism Causing Compressor Rotor-Blade Nonsynchronous Vibration-Reference-Cited by-同舟云学术

Investigation of Flow Instability Mechanism Causing Compressor Rotor-Blade Nonsynchronous Vibration

Published:2014-09 Issue:9 Volume:52 Page:2019-2031
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Im Hongsik¹,Zha Gecheng¹

Affiliation:

1. Dept. of Mechanical and Aerospace Engineering, University of Miami, Coral Gables, Florida 33124

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052781

Reference30 articles.

1. KielbR.ThomasJ.BarterP.HallK. “Blade Excitation by Aerodynamic Instabilites—A Compressor Blade Study,” American Soc. of Mechanical Engineers Paper GT-2003-38634, 2003.

2. An Experimental and Numerical Investigation into the Mechanisms of Rotating Instability

3. MailachR.LehmannI.VogelerK. “Rotating Instabilites in an Axial Compressor Originating From the Fluctuating Blade Tip Vortex,” American Soc. of Mechanical Engineers Paper GT-2003-38634, 2003.

4. Blade Tip Clearance Flow and Compressor Nonsynchronous Vibrations: The Jet Core Feedback Theory as the Coupling Mechanism

5. The Tip Clearance Flow Resonance Behind Axial Compressor Nonsynchronous Vibration

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