Abstract
Optimization problems in many industrial applications are very hard to solve. Many examples of them can be found in the design of aeronautical systems. In this field, the designer is frequently faced with the problem of considering not only a single design objective, but several of them, i.e., the designer needs to solve a Multi-Objective Optimization Problem (MOP). In aeronautical systems design, aerodynamics plays a key role in aircraft design, as well as in the design of propulsion system components, such as turbine engines. Thus, aerodynamic shape optimization is a crucial task, and has been extensively studied and developed. Multi-Objective Evolutionary Algorithms (MOEAs) have gained popularity in recent years as optimization methods in this area, mainly because of their simplicity, their ease of use and their suitability to be coupled to specialized numerical simulation tools. In this chapter, we will review some of the most relevant research on the use of MOEAs to solve multi-objective and/or multi-disciplinary aerodynamic shape optimization problems. In this review, we will highlight some of the benefits and drawbacks of the use of MOEAs, as compared to traditional design optimization methods. In the second part of the chapter, we will present a case study on the application of MOEAs for the solution of a multi-objective aerodynamic shape optimization problem.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Anderson, M.B.: Genetic Algorithm. In: Aerospace Design: Substantial Progress, Tremendous Potential. Technical report, Sverdrup Technology Inc./TEAS Group, 260 Eglin Air Force Base, FL 32542, USA (2002)
Arabnia, M., Ghaly, W.: A Strategy for Multi-Objective Shape optimization of Turbine Stages in Three-Dimensional Flow. In: 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Victoria, British Columbia Canada, September 10 –12 (2008)
AriasMontano, A., Coello, C.A.C., Mezura-Montes, E.: MODE-LD+SS: A Novel Differential Evolution Algorithm Incorporating Local Dominance and Scalar Selection Mechanisms for Multi-Objective Optimization. In: 2010 IEEE Congress on Evolutionary Computation (CEC 2010), Barcelona, Spain, IEEE Press, Los Alamitos (2010)
Benini, E.: Three-Dimensional Multi-Objecive Design optimization of a ransonic Compressor Rotor. Journal of Propulsin and Power 20(3), 559–565 (2004)
Beume, N., Naujoks, B., Emmerich, M.: SMS-EMOA: Multiobjective SelectionBasd on Dominated Hypervolume. European Journal of Operational Research 181, 1653–1659 (2007)
Chiba, K., Jeong, S., Obayashi, S., Yamamoto, K.: Knowledge Discovery in Aerodynamic Design Space for Flyback–Booster Wing Using Data Mining. In: 14th AIAA/AHI Space Planes and Hypersonic System and Technologies Conference, Canberra, Australia, November 6–9 (2006)
Chiba, K., Obayashi, S., Nakahashi, K.: Design Exploration of Aerodynamic Wing Shape for Reusable Launch Vehicle Flyback Booster. Journal of Aircraft 43(3), 832–836 (2006)
Chiba, K., Oyama, A., Obayashi, S., Nakahashi, K., Morino, H.: Multidisciplinary Design Optimization and Data Mining for Transonic Regional-Jet Wing. AIAA Journal of Aircraft 44(4), 1100–1112 (2007), doi:10.2514/1.17549
Chung, H.-S., Choi, S., Alonso, J.J.: Supersonic Business Jet Design using a Knowledge-Based Genetic Algorithm with an Adaptive, Unstructured Grid Methodology. In: AIAA Paper 2003-3791, 21st Applied Aerodynamics Conference, Orlando, Florida, USA, June 23-26 (2003)
Coello, C.A.C.: Theoretical and Numerical Constraint Handling Techniques used with Evolutionary Algorithms: A Survey of the State of the Art. Computer Methods in Applied Mechanics and Engineering 191(11-12), 1245–1287 (2002)
Deb, K.: Multi-Objective Optimization using Evolutionary Algorithms. John Wiley & Sons, Chichester (2001) ISBN 0-471-87339-X
Deb, K., Pratap, A., Agarwal, S., Meyarivan, T.: A Fast and Elitist Multiobjective Genetic Algorithm: NSGA–II. IEEE Transactions on Evolutionary Computation 6(2), 182–197 (2002)
Drela, M.: XFOIL: An Analysis and Design System for Low Reynolds Number Aerodynamics. In: Conference on Low Reynolds Number Aerodynamics. University of Notre Dame, IN (1989)
Fonseca, C.M., Fleming, P.J.: Genetic Algorithms forMultiobjective Optimization: Formulation, Discussion and Generalization. In: Stephanie, F. (ed.) Proceedings of the Fifth International Conference on Genetic Algorithms, pp. 416–423. University of Illinois at Urbana-Champaign, Morgan Kauffman Publishers, San Mateo, California (1993)
Gonzalez, L.F.: Robust Evolutionary Methods forMulti-objective and Multidisciplinary Design Optimization in Aeronautics. PhD thesis, School of Aerospace, Mechanical and Mechatronic Engineering, The University of Sydney, Australia (2005)
Hua, J., Kong, F., Liu, P.y., Zingg, D.: Optimization of Long-Endurance Airfoils. In: AIAA-2003-3500, 21st AIAA Applied Aerodynamics Conference, Orlando, FL, June 23-26 (2003)
Jameson, A., Caughey, D.A., Newman, P.A., Davis, R.M.: NYU Transonic Swept-Wing Computer Program - FLO22. Technical report, Langley Research Center (1975)
Jeong, S., Chiba, K., Obayashi, S.: DataMining for erodynamic Design Space. In: AIAA Paper 2005–5079, 23rd AIAA Applied Aerodynamic Conference, Toronto Ontario Canada, June 6–9 (2005)
Jin, Y.: A comprehensive survey of fitness approximation in evolutionary computation. Soft Computing 9(1), 3–12 (2005)
Kroo, I.: Multidisciplinary Optimization Applications in Preliminary Design – Status and Directions. In: 38th, and AIAA/ASME/AHS Adaptive Structures Forum, Kissimmee, FL, April 7-10 (1997)
Kroo, I.: Innovations in Aeronautics. In: 42nd AIAA Aerospace Sciences Meeting, Reno, NV, January 5-8 (2004)
Kuhn, T., Rösler, C., Baier, H.: Multidisciplinary Design Methods for the Hybrid Universal Ground Observing Airship (HUGO). In: AIAA Paper 2007–7781, Belfast, Northern Ireland, September 18-20 (2007)
Lee, D.S., Gonzalez, L.F., Srinivas, K., Auld, D.J., Wong, K.C.: Erodynamics/RCS Shape Optimisation of Unmanned Aerial Vehicles using Hierarchical Asynchronous Parallel Evolutionary Algorithms. In: AIAA Paper 2006-3331, 24th AIAA Applied Aerodynamics Conference, San Francisco, California, USA, June 5-8 (2006)
Lee, D.S., Gonzalez, L.F., Periaux, J., Srinivas, K.: Robust Design Optimisation Using Multi-Objective Evolutionary Algorithms. Computer & Fluids 37, 565–583 (2008)
Leifsson, L., Koziel, S.: Multi-fidelity design optimization of transonic airfoils using physics-based surrogate modeling and shape-preserving response prediction. Journal of Computational Science, 98–106 (2010)
Lian, Y., Liou, M.-S.: Multiobjective Optimization Using Coupled Response Surface Model end Evolutinary Algorithm. In: AIAA Paper 2004–4323, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, , Albany, New York, USA, August 30-September 1 (2004)
Lian, Y., Liou, M.-S.: Multi-Objective Optimization of Transonic Compressor Blade Using Evolutionary Algorithm. Journal of Propulsion and Power 21(6), 979–987 (2005)
Liao, W., Tsai, H.M.: Aerodynamic Design optimization by the Adjoint Equation Method on Overset Grids. In: AIAA Paper 2006-54, 44th AIAA Aerospace Science Meeting and Exhibit, Reno, Nevada, USA, January 9-12 (2006)
Mezura-Montes, E. (ed.): Constraint-Handling in Evolutionary Optimization. SCI, vol. 198. Springer, Heidelberg (2009)
Mialon, B., Fol, T., Bonnaud, C.: Aerodynamic Optimization Of Subsonic Flying Wing Configurations. In: AIAA-2002-2931, 20th AIAA Applied Aerodynamics Conference, St. Louis Missouri, June 24-26 (2002)
Obayashi, S., Tsukahara, T.: Comparison of OptimizationAlgorithms for Aerodynamic Shape Design. In: AIAA-96-2394-CP, AIAA 14th Applied Aerodynamics Conference, New Orleans, LA, USA, June 17-20 (1996)
Ong, Y.-S., Nair, P.B., Lum, K.Y.: Max-min surrogate-assisted evolutionary algorithm for robust design. IEEE Trans. Evolutionary Computation 10(4), 392–404 (2006)
Oyama, A.: Wing Design Using Evolutionary Algorithms. PhD thesis, Department of Aeronautics and Space Engineering. Tohoku University, Sendai, Japan (March 2000)
Oyama, A., Nonomura, T., Fujii, K.: Data Mining of Pareto-Optimal Transonic Airfoil Shapes Using Proper Orthogonal Decomposition. AIAA Journal Of Aircraft 47(5), 1756–1762 (2010)
Oyama, A., Okabe, Y., Shimoyama, K., Fujii, K.: Aerodynamic Multiobjective Design Exploration of a Flapping Airfoil Using a Navier-Stokes Solver. Journal Of Aerospace Computing, Information, and Communication 6(3), 256–270 (2009)
Price, K.V., Storn, R., Lampinen, J.A.: Differential Evolution. A Practical Approach to Global Optimization. Springer, Berlin (2005)
Rai, M.M.: Robust Optimal Design With Differential Evolution. In: AIAA Paper 2004- 4588, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany, New York, USA, August 30 - September 1 (2004)
Ray, T., Tsai, H.M.: A Parallel Hybrid Optimization Algorithm for Robust Airfoil Design. In: AIAA Paper 2004–905, 42nd AIAA Aerospace Science Meeting and Exhibit, Reno, Nevada, USA, January 5 -8 (2004)
Sierra, M.R., Coello, C.A.C.: A Study of Fitness Inheritance and ApproximationTechniques for Multi-Objective Particle Swarm Optimization. In: 2005 IEEE Congress on Evolutionary Computation (CEC 2005), vol. 1, pp. 65–72. IEEE Service Center, Edinburgh (2005)
Sasaki, D., Obayashi, S.: Efficient search for trade-offs by adaptive range multiobjective genetic algorithm. Journal Of Aerospace Computing, Information, and Communication 2(1), 44–64 (2005)
Sasaki, D., Obayashi, S., Nakahashi, K.: Navier-Stokes Optimization of Supersonic Wings with Four Objectives Using Evolutionary Algorithms. Journal Of Aircraft 39(4), 621–629 (2002)
Secanell, M., Suleman, A.: Numerical Evaluation of Optimization Algorithms for Low-Reynolds Number Aerodynamic Shape Optimization. AIAA Journal 10, 2262–2267 (2005)
Shimoyama, K., Oyama, A., Fujii, K.: A New Efficient and Useful Robust Optimization Approach –Design forMulti-objective Six Sigma. In: 2005 IEEE Congress on Evolutionary Computation (CEC 2005), vol. 1, pp. 950–957. IEEE Service Center, Edinburgh (2005)
Shimoyama, K., Oyama, A., Fujii, K.: Development of Multi-Objective Six-Sigma Approach for Robust Design Optimization. Journal of Aerospace Computing, Information, and Communication 5(8), 215–233 (2008)
Sobieczky, H.: Parametric Airfoils and Wings. In: Fuji, K., Dulikravich, G.S. (eds.) Notes on Numerical Fluid Mechanics, vol. 68, pp. 71–88. Vieweg Verlag, Wiesbaden (1998)
Song, W., Keane, A.J.: Surrogate-based aerodynamic shape optimization of a civil aircraft engine nacelle. AIAA Journal 45(10), 265–2574 (2007), doi:10.2514/1.30015
Srinivas, N., Deb, K.: Multiobjective Optimization Using Nondominated Sorting in Genetic Algorithms. Evolutionary Computation 2(3), 221–248 (1994)
Szöllös, A., Smíd, M., Hájek, J.: Aerodynamic optimization via multiobjective micro-genetic algorithm with range adaptation, knowledge-based reinitialization, crowding and epsilon-dominance. Advances in Engineering Software 40(6), 419–430 (2009)
Tani, N., Oyama, A., Okita, K., Yamanishi, N.: Feasibility study of multi objective shape optimization for rocket engine turbopump blade design. In: 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, July 21 - 23 (2008)
Tsutsui, S., Ghosh, A.: Genetic algorithms with a robust solution searching scheme. IEEE Trans. Evolutionary Computation 1(3), 201–208 (1997)
Yamaguchi, Y., Arima, T.: Multi-Objective Optimization for the Transonic Compressor Stator Blade. In: AIAA Paper 2000–4909, 8th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, AIAA Paper 2000–4909, 8th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, September 6 - 8, Long Beach, CA, USA (2000)
Zhang, Q., Li, H.: MOEA/D: A Multiobjective Evolutionary Algorithm Based on Decomposition. IEEE Transactions on Evolutionary Computation 11(6), 712–731 (2007)
Zitzler, E., Thiele, L.: Multiobjective Evolutionary Algorithms: A Comparative Case Study and the Strength Pareto Approach. IEEE Transactions on Evolutionary Computation 3(4), 257–271 (1999)
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2011 Springer-Verlag Berlin Heidelberg
About this chapter
Cite this chapter
Arias-Montaño, A., Coello Coello, C.A., Mezura-Montes, E. (2011). Evolutionary Algorithms Applied to Multi-Objective Aerodynamic Shape Optimization. In: Koziel, S., Yang, XS. (eds) Computational Optimization, Methods and Algorithms. Studies in Computational Intelligence, vol 356. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-20859-1_10
Download citation
DOI: https://doi.org/10.1007/978-3-642-20859-1_10
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-20858-4
Online ISBN: 978-3-642-20859-1
eBook Packages: EngineeringEngineering (R0)