Prediction of Aerodynamically Induced Blade Vibrations in a Radial Turbine Rotor Using the Nonlinear Harmonic Approach
Author:
Affiliation:
1. ITSM—Institute of Thermal Turbomachinery and Machinery Laboratory, University of Stuttgart, Stuttgart 70569, Germany e-mail:
2. ITSM—Institute of Thermal Turbomachinery and Machinery Laboratory, University of Stuttgart, Stuttgart 70569, Germany
Abstract
Funder
Forschungsvereinigung Verbrennungskraftmaschinen
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.4040856/6183556/gtp_141_02_021007.pdf
Reference15 articles.
1. Müller, T. R., Vogt, D. M., Vogel, K., Phillipsen, B. A., and Hönisch, P., 2017, “Influence of Detailing on Aerodynamic Forcing of a Transonic Axial Turbine Stage and Forced-Response Prediction for Low-Engine-Order (LEO) Excitation,” ASME Paper No. GT2017-64502.10.1115/GT2017-64502
2. Calculation of Unsteady Wake/Rotor Interaction;J. Propul. Power,1988
3. Clark, J. P., Stetson, G. M., Magge, S. S., Ni, R. H., Haldemann, C. W., and Dunn, M. G., 2000, “The Effect of Airfoil Scaling on the Predicted Unsteady Loading on the Blade of a 1 and 1/2 Stage Transonic Turbine and a Comparison With Experimental Results,” ASME Paper No. 2000-GT-0446.10.1115/2000-GT-0446
4. Effect of Scaling of Blade Row Sectors on the Prediction of Aerodynamic Forcing in Highly-Loaded Transonic Compressor Stage;ASME. J. Turbomach.,2009
5. Fourier Methods for Turbomachinery Applications;Prog. Aerosp. Sci.,2010
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