![Computational Fluid Dynamics of Compressor Blades Within a Gas Turbine Engine (HiPSTAR) - Computational Modelling Group Computational Fluid Dynamics of Compressor Blades Within a Gas Turbine Engine (HiPSTAR) - Computational Modelling Group](https://cmg.soton.ac.uk/media/project-images/288/presure.png)
Computational Fluid Dynamics of Compressor Blades Within a Gas Turbine Engine (HiPSTAR) - Computational Modelling Group
![Applied Sciences | Free Full-Text | Effect of Slot at Blade Root on Compressor Cascade Performance under Different Aerodynamic Parameters Applied Sciences | Free Full-Text | Effect of Slot at Blade Root on Compressor Cascade Performance under Different Aerodynamic Parameters](https://www.mdpi.com/applsci/applsci-06-00421/article_deploy/html/images/applsci-06-00421-g001.png)
Applied Sciences | Free Full-Text | Effect of Slot at Blade Root on Compressor Cascade Performance under Different Aerodynamic Parameters
![High-Speed Axial Compressor – Institute of Turbomachinery and Fluid Dynamics – Leibniz University Hannover High-Speed Axial Compressor – Institute of Turbomachinery and Fluid Dynamics – Leibniz University Hannover](https://www.tfd.uni-hannover.de/fileadmin/tfd/seitenvorlagen/Dateien/Leistungsspektrum/Versuchsstaende/Hochgeschwindigkeits-Axialverdichter/csm_Rotorkonfiguration_4146afc528.jpg)