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aerodynamics - Why is a centrifugal compressor in aircraft engine less susceptible to stall and surge? - Aviation Stack Exchange
![IJTPP | Free Full-Text | Surge Margin Optimization of Centrifugal Compressors Using a New Objective Function Based on Local Flow Parameters IJTPP | Free Full-Text | Surge Margin Optimization of Centrifugal Compressors Using a New Objective Function Based on Local Flow Parameters](https://www.mdpi.com/ijtpp/ijtpp-04-00042/article_deploy/html/images/ijtpp-04-00042-g001.png)
IJTPP | Free Full-Text | Surge Margin Optimization of Centrifugal Compressors Using a New Objective Function Based on Local Flow Parameters
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