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    Numerical Simulation of the Flow Pulsations Origin in Cascades of the Rear Blade Rows in a Gas Turbine Axial Compressor Using Low Calorific Fuel 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 003:;page 31012
    Author(s): Vaclav Cyrus; Jiri Polansky
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Fatigue failure of the last three stator rows vanes (S17, EGV1, and EGV2) in the 17 stage gas turbine axial compressor occurred in the power plant where low calorific fuel syngas, was used. ...
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