Mechanical Sciences
Mechanical Sciences
Mechanical Sciences
Articles | Volume 8, issue 1
Articles | Volume 8, issue 1
https://doi.org/10.5194/ms-8-127-2017
© Author(s) 2017. This work is distributed under
the Creative Commons Attribution 3.0 License.
https://doi.org/10.5194/ms-8-127-2017
© Author(s) 2017. This work is distributed under
the Creative Commons Attribution 3.0 License.
Articles | Volume 8, issue 1
Research article
 | 
31 May 2017
Research article |  | 31 May 2017

Performance of a Low Speed Axial Compressor Rotor Blade Row under Different Inlet Distortions

Reza Taghavi Zenouz, Mehran Eshaghi Sir, and Mohammad Hosein Ababaf Behbahani

Viewed

Total article views: 2,067 (including HTML, PDF, and XML)
HTML PDF XML Total BibTeX EndNote
1,003 1,000 64 2,067 51 61
  • HTML: 1,003
  • PDF: 1,000
  • XML: 64
  • Total: 2,067
  • BibTeX: 51
  • EndNote: 61
Views and downloads (calculated since 31 May 2017)
Cumulative views and downloads (calculated since 31 May 2017)

Viewed (geographical distribution)

Total article views: 2,005 (including HTML, PDF, and XML) Thereof 1,998 with geography defined and 7 with unknown origin.
Country # Views %
  • 1
1
 
 
 
 

Cited

Latest update: 25 Dec 2024
Download
Short summary
Performance of gas turbine engines are strongly dependent on entrance air flow conditions. In the current work, responses of an axial compressor isolated rotor blade row to various inlet distortions are investigated utilizing computational fluid dynamic technique. Distortions are imposed by five screens of different geometries but with the same blockage ratio. Results showed that the worst cases belong to non-symmetric blockages, i.e., those of partial circumferential configurations.
Read more