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Title : OPTIMIZATION OF THE GAS TURBINE ENGINE PARTS USING METHODS OF NUMERICAL SIMULATION
Company : Sigma Technology
File Name : GT2007_28205.pdf
Size : 721177
Type : application/pdf
Date : 17-Apr-2010
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Downloads : 3

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The paper presents the results of optimizing a three-stage axial compressor. The optimization goal was to improve the compressor efficiency at two flight conditions by optimizing geometry of the 5 compressor rows (62 design parameters).
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