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Compressor blade surface waviness results from the manufacturing process.
The resulting compressor blade section is optimized w.r.t.
First, the design concept based on a 2D compressor blade profile is introduced.
The methodology has been successfully implemented on a critical aeroengine component, i.e. thin-curved compressor blade.
A compressor blade is designed with a curvature induced pressure-recovery concept.
As a result, the compressor blade achieves high loading with acceptable loss.
Similar(22)
Liquid drops can destroy compressor blades.
Typical parts include inlet cases, compressor blades, disks, and hubs, as well as spacers and seals.
The strongest and most corrosion-resistant of the group contains nickel; it has been used for gas-turbine compressor blades.
The results show that vitrified bonded tools are not suitable for the structuring of compressor blades.
This paper introduces a novel design method of highly loaded compressor blades with air injection.
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