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

Related subject area

Subject: Fluid Mechanics | Techniques and Approaches: Numerical Modeling and Analysis
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
Mech. Sci., 8, 127–136, https://doi.org/10.5194/ms-8-127-2017,https://doi.org/10.5194/ms-8-127-2017, 2017
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Cited articles

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Bardina, J. E., Huang, P. G., and Coakley, T. J.: Turbulence modeling validation, testing, and development, 28th Fluid Dynamics Conference, https://doi.org/10.2514/6.1997-2121, 1997. 
Beheshti, B. H., Teixeira, J. A., Ivey, P. C., Ghorbanian, K., and Farhanieh, B.: Parametric study of tip clearance – casing treatment on performance and stability of a transonic axial compressor, J. Turbomach., 126, 527–535, https://doi.org/10.1115/1.1791643, 2004. 
Chen, H., Huang, X., and Fu, S.: CFD investigation on stall mechanisms and casing treatment of a transonic compressor, 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, https://doi.org/10.2514/6.2006-4799, 2006. 
Choi, M.: Effects of circumferential casing grooves on the performance of a transonic axial compressor, Int. J. Turbo Jet Eng., 32, 361–371, https://doi.org/10.1515/tjj-2015-0001, 2015. 
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The performance of different models of grooves with various tip gap height on NASA rotor 37 is...
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