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1S1B first stage first blade 1S2B first stage second blade 1S3B first stage third blade 2S1B second stage first 1blade 2S2B second stage second blade B blade Comp. compressor FEA finite element analysis FEM finite element method FIV flow induced vibration GT gas turbine m/s meter per second S stage 1 Introduction Early fault finding is a major challenge in turbomachinery, especially once these are installed at their locations and are in operation.
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