Fig 20 -

Fig 20 -

<p>Changes in main blades before and after optimization: (a) Change of leading edge and middle control point of main blade, (b) Change of trailing edge control point of main blade.</p>

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Bibliographic Details
Main Author:	Yesong Wang (331723) (author)
Other Authors:	Zixuan Sun (3495020) (author), Jisheng Liu (219678) (author), Manxian Liu (20298265) (author), Yong Zhou (23772) (author)
Published:	2024
Subjects:	Biophysics Medicine Cell Biology Neuroscience Biotechnology Evolutionary Biology Computational Biology Space Science Biological Sciences not elsewhere classified Mathematical Sciences not elsewhere classified rated operating conditions objective evolutionary algorithms normal operating conditions enhancing solution quality computational fluid dynamics centrifugal impeller based centrifugal compressor blades two parameterization approaches two optimization stages optimization results demonstrate numerous design variables local mapping model global mapping model low optimization efficiency blade geometry configuration optimization design local optimization blade geometry centrifugal impellers parameterization methods optimization space isentropic efficiency enable global xlink "> thoroughly explored surge margin study presents methodology addresses inflexible configurations form deformation control bodies challenges associated bezier surfaces bezier surface aerodynamic performance
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