Study of flow control strategies combined between suction slot and vortex generator on an axial compressor cascade

Author:

Li Fengming1,Ma Shan1,Sun Xiaolin1

Affiliation:

1. Civil Aviation Flight University of China, China

Publisher

ACM

Reference11 articles.

1. Numerical investigation of inlet boundary layer skew in axial-flow compressor cascade and the corresponding non-axisymmetric end wall profiling

2. Aaron J. Pope , Andrew Oliva , Aleksandar Jemcov , Performance of a Subsonic Compressor Airfoil with Upstream , End-wall Injection Flow. Proceeding of ASME Turbo Expo , Virtual, Online , 2021 . Aaron J. Pope, Andrew Oliva, Aleksandar Jemcov, Performance of a Subsonic Compressor Airfoil with Upstream, End-wall Injection Flow. Proceeding of ASME Turbo Expo, Virtual, Online, 2021.

3. A combined application of micro-vortex generator and boundary layer suction in a high-load compressor cascade

4. About Transonic Compressor Tandem Design: A Principle Study

5. Payyappalli M M , Pradeep A M. Effect of Tandem Blading in Contra-Rotating Axial Flow Fans . Proceeding of ASME Turbo Expo , Oslo, Norway , 2018 . Payyappalli M M, Pradeep A M. Effect of Tandem Blading in Contra-Rotating Axial Flow Fans. Proceeding of ASME Turbo Expo, Oslo, Norway, 2018.

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