Forced Response Excitation Due to the Stator Vanes of Two and Three Compressor Stages Away
Author:
Affiliation:
1. Technical Institute, Kawasaki Heavy Industries, Co., Ltd., Akashi, Hyogo 673 8666, Japan
2. Aerospace Systems Company, Kawasaki Heavy Industries, Co., Ltd., Akashi, Hyogo 673 8666, Japan
Abstract
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/143/11/111018/6765917/gtp_143_11_111018.pdf
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3. Prediction of Low-Engine-Order Excitation Due to a Nonsymmetrical Nozzle Ring in a Radial Turbine by Means of the Nonlinear Harmonic Approach;ASME J. Eng. Gas Turbines Power,2019
4. Forced Response Analysis of a Radial Turbine With Different Modeling Methods,2019
5. Hydro Francis Runner Stability and Forced Response Calculations,2019
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