Stall Margin Enhancement of Aeroengine Compressor with a Novel Type of Alternately Swept Blades
International conference on aerospace system science and engineering
01.01.2020
12 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Stall Margin Enhancement of Aeroengine Compressor with a Novel Type of Alternately Swept Blades
Springer Verlag | 2020
|An Investigation on Rotating Stall in an Aeroengine Transonic Compressor with Inlet Distortion
Springer Verlag | 2022
|An Investigation on Rotating Stall in an Aeroengine Transonic Compressor with Inlet Distortion
British Library Conference Proceedings | 2023
|