Articles | Volume 11, issue 1
https://doi.org/10.5194/ms-11-153-2020
https://doi.org/10.5194/ms-11-153-2020
Research article
 | 
12 May 2020
Research article |  | 12 May 2020

Axial transonic compressor performance enhancement with circumferential grooves

Naseem Ahmad, Qun Zheng, Hamza Fawzy, Tasneem Yaqoob, Salman Abdu Ahmad, and Jiang Bin

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Latest update: 04 Sep 2026
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Short summary
The performance of different models of grooves with various tip gap height on NASA rotor 37 is investigated by discretizing 3D RANS equations based on finite volume technique. Rectangular circumferential grooves casing treatment (CGCT) profile and smooth wall casing performances are evaluated. Moreover, the adiabatic efficiencies and the stall margins of smooth wall casing, rectangular grooves and rectangular grooves with fillet and chamfer corners are compared to assess the impacts of profiles
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