بهینه‌سازی عملکرد کمپرسور جریان محوری با تغییر زوایای لین و سوییپ

[1]      Yuan X., Tanuma T., Zhu X., Lin Z. and Nomura D., A CFD approach to fluid dynamic optimum design of steam turbine stages with stator and rotor blades, ASME Turbo-Expo, GT2010-22477, 2010.

[2]     Fathi A. and Shadaram A., Optimization of a 10-stage axial flow compressor using streamline curvature method with respect to aerodynamic criteria, Modares Mechanical Engineering, Vol. 12, No. 2, pp. 72-86, 1391.

[3]     Azizi R., Ebrahimi R. and Ziabasharhagh M., The novel preliminary design algorithm of multistage axial compressors through two layer multi-objective/multi-variables optimization, Modares Mechanical Engineering, Vol. 13, No. 12, pp. 1-13, 1392.

[4]  بزاززاده م.، دهقان منشادی م. و کرباسی زاده م.، بررسی عددی تاثیر نسبت فشاری بر پدیده تداخل موج ضربه‌ای و لایه مرزی در یک مجرا با سطح مقطع ثابت . مجلۀ مهندسی مکانیک دانشگاه تبریز، د. 47، ش. 3، ص 51-60، 1396.

[5]     Oyama A., Liou M.S. and Obayashi S., Transonic axial-flow blade shape optimization using evolutionary algorithm and three-dimensional Navier-Stokes solver, AIAA 2002-5642. vol. 4. Citeseer, 2002.

[6]     Pierret S., Multi-objective and multi-disciplinary optimization of three-dimensional turbomachinery blades, Proceedings of the 6th World Congresses of Structural and Multidisciplinary Optimization, 2005.

[7]     Choon-Man J., Abudus S. and Kwang-Yong K., Optimal design of swept, leaned and skewed blades in a transonic axial compressor, ASME Turbo-Expo, GT2006-90384, 2006.

[8]     Keskin A., Dutta A. K. and Bestle D., Modern compressor aerodynamic blading process using multi-objective optimization, ASME Turbo-Expo, GT2006-90206, 2006. 

[9]     Huppertz A., Flassig P.M., Flassig R.J. and Swoboda M., Knowledge-based 2d blade design using multi-objective aerodynamic optimization and a neural network, ASME Turbo-Expo, GT2007-28204, 2007.

[10] Cardamone P., Aerodynamic Optimization of Highly Loaded Turbine Cascade Blades for Heavy Duty Gas Turbine Applications,  Thesis, Universität der Bundeswehr München, Universitätsbibliothek, 2006.

[11]  Pierret S. and Van den Braembussche R., Turbomachinery blade design using a Navier–Stokes solver and artificial neural network, Journal of Turbomachinery, Vol. 121, pp. 326,1999.

[12]  Mengistu T. and Ghaly W., Aerodynamic optimization of turbomachinery blades using evolutionary methods and ANN-based surrogate models, Optimization and Engineering, Vol. 9, No. 3, pp. 239-255, 2008.

[13]  Kim J. H., Choi J. H. and Kim K. Y., Design optimization of a centrifugal compressor impeller using radial basis neural network method, ASME Turbo-Expo, GT2009-59666, 2009

[14]  Thévenin D., Janiga G. and NetLibrary I., Optimization and computational fluid dynamics: Springer Verlag, 2008.

[15]  Chipperfied A., Fleming P., Pohlheim H.and Fonseca C., Genetic Algorithm Toolbox for use with Matlab, University of Sheffield,  2001.

[16]  Pourfarzaneh H., Hajilouy-Benisi A., Farshchi M., Zero-dimensional modeling of axial and centrifugal compressors of a turbojet and validation by test results, Sharif Mechanical Engineering, Vol. 28, No. 3, pp. 23-27, 1391.