A Low-Speed Compressor Test Rig for Flutter Investigations
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, Technische Universität Berlin, Marchstr. 12-14, Berlin 10587, Germany e-mail:
2. German Aerospace Center, Institute of Aeroelasticity, Bunsenstraße 10, Göttingen 37073, Germany e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4041817/6311025/turbo_141_05_051009.pdf
Reference22 articles.
1. Vogt, D., 2005, “Experimental Investigation of Three-Dimensional Mechanisms in Low-Pressure Turbine Flutter,” Ph.D. thesis, Royal Institute of Technology, Stockholm, Sweden.http://www.diva-portal.org/smash/get/diva2:7902/FULLTEXT01.pdf
2. System Mode Shapes in the Flutter of Compressor Blade Rows;J. Aeronaut. Sci.,1956
3. Aeroelastic Formulations for Turbomachines and Propellers,1988
4. Investigation of Blade Flutter in a Subsonic Turbine,1976
5. Urban, B., Stetter, H., and Vortmeyer, N., 2000, “Experimental Investigation of Shock-Induced Blade Oscillation at an Elastically Suspended Turbine Cascade in Transonic Flow,” ASME Paper No. 2000-GT-378.10.1115/2000-GT-0378
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