Surrogate-Based Shape Optimization of Stall Margin and Efficiency of a Centrifugal Compressor

Author:

Khalfallah Smail1,Ghenaiet Adel2,Benini Ernesto3,Bedon Gabriele3

Affiliation:

1. Applied Mechanics, Laboratory of Thermal Power Systems, 16046 Algiers, Algeria

2. Faculty of Mechanical Engineering, University of Sciences and Technology Houari Boumediene, 16111 El-Alia, Algiers, Algeria

3. Department of Industrial Engineering, University of Padova, 35131 Padova, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference31 articles.

1. LohnerR., Applied CFD Techniques: An Introduction Based on Finite Element Methods, 2nd ed., Wiley, Hoboken, NJ, 2008, pp. 449–480.

2. Multi-objective optimization of turbomachinery using improved NSGA-II and approximation model

3. DebK., Optimization for Engineering Design, Algorithms and Examples, Prentice–Hall, Upper Saddle River, NJ, 1995, pp. 1–142.

4. Multi-objective optimization of an axial compressor blade

5. Aerodynamic optimization of turbomachinery blades using evolutionary methods and ANN-based surrogate models

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