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Investigations on a Radial Compressor Tandem-Rotor Stage With Adjustable Geometry
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A radial compressor stage has been investigated mainly experimentally for aerodynamic stage optimization. The rotor (πt = 3.9) consists of a profiled axial inducer and a conventionally designed ...
Improved Compressor Exit Diffuser for an Industrial Gas Turbine
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Cycle studies carried out for the medium pressure ratio gas turbine THM 1304 of 10 MW power output manufactured by MAN Turbomaschinen AG GHH BORSIG predicted that the overall efficiency of ...
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