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

Viewed

Total article views: 1,623 (including HTML, PDF, and XML)
HTML PDF XML Total BibTeX EndNote
1,299 304 20 1,623 17 14
  • HTML: 1,299
  • PDF: 304
  • XML: 20
  • Total: 1,623
  • BibTeX: 17
  • EndNote: 14
Views and downloads (calculated since 12 May 2020)
Cumulative views and downloads (calculated since 12 May 2020)

Viewed (geographical distribution)

Total article views: 1,449 (including HTML, PDF, and XML) Thereof 1,362 with geography defined and 87 with unknown origin.
Country # Views %
  • 1
1
 
 
 
 

Cited

Latest update: 18 Apr 2024
Download
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