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Applied Sciences | Free Full-Text | Preliminary Optimization of Multi-Stage Axial-Flow Industrial Process Compressors Using Aero-Engine Compressor Design Strategy
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IJTPP | Free Full-Text | A Casing Treatment with Axial Grooves for Centrifugal Compressors
Performance deterioration of axial compressor rotor due to uniform and non-uniform surface roughness - Ashima Malhotra, Shraman Goswami, Pradeep Amboor Madathil, 2022
Applied Sciences | Free Full-Text | A Study on the Stall Detection of an Axial Compressor through Pressure Analysis
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PDF] Design and Development of a 12:1 Pressure Ratio Compressor for the Ruston 6-MW Gas Turbine | Semantic Scholar
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jet engine - Decreasing Area of Axial Compressor - Aviation Stack Exchange
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SOLVED: (c) An A10 stage axial flow compressor develops an overall pressure ratio of 8.0 with an isentropic efficiency of 0.85. The absolute velocity component of air enters the rotor at an