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

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Latest update: 20 Nov 2024
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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.
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