CFD Investigation on Stall Mechanisms and Casing Treatment of a Transonic Compressor
Author:
Publisher
American Institute of Aeronautics and Astronautics
Reference8 articles.
1. The Role of Tip Clearance in High-Speed Fan Stall
2. The Effect of Tip Clearance on a Swept Transonic Compressor Rotor
3. Development of Hub Corner Stall and Its Influence on the Performance of Axial Compressor Blade Rows
4. Calculation of Tip Clearance Effects in a Transonic Compressor Rotor
5. Recommendations for Achieving Accurate Numerical Simulation of Tip Clearance Flows in Transonic Compressor Rotors
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1. Aerodynamic Optimization of a Single-Stage Transonic Axial Compressor with a Circumferential Feedback Channel;Journal of Aerospace Engineering;2024-05
2. Numerical optimization of a stator blade to enhance aerodynamic performance in a transonic fan stage;European Journal of Mechanics - B/Fluids;2024-01
3. An Intellectual Aerodynamic Design Method for Compressors Based on Deep Reinforcement Learning;Aerospace;2023-02-13
4. A Combined Artificial-Intelligence Aerodynamic Design Method for a Transonic Compressor Rotor Based on Reinforcement Learning and Genetic Algorithm;Applied Sciences;2023-01-12
5. AXIAL TRANSONIC COMPRESSOR STALL MECHANISM WITH DIFFERENT ROTATIONAL SPEEDS;Journal of Theoretical and Applied Mechanics;2022-06-08
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