Aerodynamic Optimization of Turbomachinery Cascades Using Euler/Boundary-Layer Coupled Genetic Algorithms

Öksüz, Özhan; Akmandor, I. Sinan; Kavsaoğlu, Mehmet Şerif

doi:10.2514/2.5979

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2024

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Cited by 12 publications

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“…A global optimization method based on genetic algorithm or intelligent genetic algorithm is expected to shorten and simplify the iterative design process and improve the design output. A similar approach has been previously used for aerodynamic optimization of turbo machinery cascades [1], and very good results were obtained. Glaurt [2] neglected the drag of airfoil and offered a popular theory for optimizing the airfoil.…”

Section: Introductionmentioning

confidence: 73%