Effect of radial inflow distortion on the performance of a highly loaded tandem stage
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DOI: 10.1177/09576509211031680
Abstract: Engine size and weight optimization have always been high-priority design objectives for designers. Compressors occupy a relatively large part of the gas turbine engine. Owing to the adverse pressure gradient in the compressor, achieving the… read more here.
Keywords: tandem stage; effect radial; distortion; performance ... See more keywords