Optimization of compressor blades for aircraft engines
Introduction to the optimization of axial flow compressor blades developed jointly by FRIENDSHIP Corporation and RRD Corporation.
Aircraft engine manufacturers are working daily on product development to meet the stringent demands of reducing exhaust emissions and fuel consumption. This effort requires further improvements in the design process to efficiently create aerodynamically superior compressor designs. In recent years, developing appropriate blade shapes that meet global design and performance requirements with high efficiency has necessitated numerous iterative calculations between different software tools for shape creation and fluid analysis. *For more detailed information, please refer to the related links. For further details, you can download the PDF or feel free to contact us.*
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