Multi-Level Multi-Objective Multi-Point Optimization System for Axial Flow Compressor 2D Blade Design
Author:
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
http://link.springer.com/content/pdf/10.1007/s13369-012-0435-7.pdf
Reference19 articles.
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3. Keshin, A.; Dutta, A.K.; Bestle, D.: Modern compressor aerodynamic blading process using multi-objective optimization. ASME Turbo Expo, No.GT2006-90206 (2006)
4. Bonnaiuti, D.; Zangeneh, M.: On the coupling of inverse design and optimization techniques for the multiobjective, multipoint design of turbomachinery blades. J. Turbomach. 131(021014) (2009)
5. Korakiantis, T.: Hierarchical development of three direct-design methods for two-dimensional axial-turbomachinery cascades. J. Turbomach. 115(021014), 314–324 (1993)
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