Technical Papers
Aug 28, 2017

Gradient-Enhanced Hierarchical Kriging Model for Aerodynamic Design Optimization

Publication: Journal of Aerospace Engineering
Volume 30, Issue 6

Abstract

A cokriging model incorporating gradient information and the function value of sample points can reduce the computational cost with a given level of accuracy. In this paper, the hierarchical kriging, a recently proposed cokriging method is employed, and a new method called gradient-enhanced hierarchical kriging (GEHK) is developed. First of all, a low-fidelity kriging model is built using derived samples, which are obtained by Taylor approximation using gradients and selected step sizes. Then a high-fidelity model is built by adjusting the low-fidelity kriging model with initial sample points. The GEHK model is more efficient than the traditional gradient-based cokriging model in the aerodynamic optimization, and could get a better optimum value. Taking the advantage of the modeling strategy, the global accuracy of the GEHK is not sensitive to step sizes, and the accuracy of prediction is enhanced evidently. The GEHK method is able to overcome limitations of traditional gradient-based cokriging models, and the prediction accuracy of the model is improved globally.

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Acknowledgments

This research was sponsored by the National Natural Science Foundation of China (NSFC) under Grant No. 11272263.

References

Ahn, J., Kim, H. J., Lee, D. H., and Rho, O. H. (2001). “Response surface method for airfoil design in transonic flow.” J. Aircr., 38(2), 231–238.
Booker, A. J., Dennis, J., Jr., Frank, P. D., Serafini, D. B., and Torczon, V. (1998). “Optimization using surrogate objectives on a helicopter test example.” Computational methods for optimal design and control, Springer, New York, 49–58.
Chung, H. S., and Alonso, J. (2002). “Using gradients to construct cokriging approximation models for high-dimensional design optimization problems.” 40th AIAA Aerospace Sciences Meeting and Exhibit, American Institute of Aeronautics and Astronautics, Reston, VA.
Cook, P., Firmin, M., and McDonald, M. (1977). Aerofoil RAE 2822: Pressure distributions, and boundary layer and wake measurements, Royal Aircraft Establishment, Farnborough, U.K.
Cressie, N. A. C. (1993). Statistics for spatial data, Wiley, New York.
David, J. T., Bressloff, N. W., and Keane, A. J. (2008). “Kriging hyperparameter tuning strategies.” AIAA J., 46(5), 1240–1252.
Degand, C., and Farhat, C. (2002). “A three-dimensional torsional spring analogy method for unstructured dynamic meshes.” Comput. Struct., 80(3), 305–316.
Economon, T. D., Palacios, F., and Alonso, J. J. (2012). “Optimal shape design for open rotor blades.” 30th AIAA Applied Aerodynamics Conf., American Institute of Aeronautics and Astronautics, Reston, VA, 3018.
Forrester, A. I. J., Sóbester, A., and Keane, A. J. (2007). “Multi-fidelity optimization via surrogate modelling.” Proc., Royal Soc. A, 463(2088), 3251–3269.
Han, Z. H., and Görtz, S. (2012). “Hierarchical kriging model for variable-fidelity surrogate modeling.” AIAA J., 50(9), 1885–1896.
Han, Z. H., Görtz, S., and Zimmermann, R. (2013). “Improving variable-fidelity surrogate modeling via gradient-enhanced kriging and a generalized hybrid bridge function.” Aerosp. Sci. Technol., 25(1), 177–189.
Jameson, A., Martinelli, L., and Pierce, N. A. (1998). “Optimum aerodynamic design using the Navier-Stokes equations.” Theor. Comput. Fluid Dyn., 10(1–4), 213–237.
Jameson, A., Schmidt, W., and Turkel, E. (1981). “Numerical solutions of the Euler equations by finite volume methods using Runge-Kutta time-stepping schemes.” 14th Fluid and Plasma Dynamics Conf., American Institute of Aeronautics and Astronautics, Reston, VA, 1259.
Jeong, S., Murayama, M., and Yamamoto, K. (2005). “Efficient optimization design method using kriging model.” J. Aircr., 42(5), 1375.
Jones, D. R. (2001). “A taxonomy of global optimization methods based on response surfaces.” J. Global Optim., 21(4), 345–383.
Jones, D. R., Schlonlau, M., and Welch, W. J. (2008). “Efficient global optimization of expensive black-box functions”. J. Global Optim., 13(4), 455–492.
Kanazaki, M., Tanaka, K., Jeong, S., and Yamamoto, K. (2007). “Multi-objective aerodynamic exploration of elements’ setting for high-lift airfoil using kriging model.” J Aircr., 44(3), 858–864.
Kennedy, M. (2000). “Predicting the output from a complex computer code when fast approximations are available.” Biometrika, 87(1), 1–13.
Knill, D. L., et al. (1999). “Response surface models combining linear and Euler aerodynamics for supersonic transport design.” J. Aircr., 36(1), 75–86.
Laurenceau, J., Meaux, M., Montagnac, M., and Sagaut, P. (2010). “Comparison of gradient-based and gradient-enhanced response-surface-based optimizers.” AIAA J., 48(5), 981–994.
Laurenceau, J., and Sagaut, P. (2008). “Building efficient response surfaces of aerodynamic functions with kriging and cokriging.” AIAA J., 46(2), 498–507.
Lewis, R. (1998). “Using sensitivity information in the construction of kriging models for design optimization.” 7th AIAA/USAF/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, American Institute of Aeronautics and Astronautics, Reston, VA.
Liu, W., and Batill, S. (2002). “Gradient-enhanced response surface approximations using kriging models.” 9th AIAA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, American Institute of Aeronautics and Astronautics, Reston, VA.
Madavan, M., Rai, M., and Huber, F. (1998). “Neural net-based redesign of a gas generator turbine for improved unsteady aerodynamic performance.” 35th Joint Propulsion Conf. and Exhibit, Joint Propulsion Conf., American Institute of Aeronautics and Astronautics, Reston, VA.
Madsen, J. I., Shyy, W., and Haftka, R. T. (2000). “Response surface techniques for diffuser shape optimization.” AIAA J., 38(9), 1512–1518.
MATLAB [Computer software]. MathWorks, Natick, MA.
McDonald, D. B., Grantham, W. J., Tabor, W. L., and Murphy, M. J. (2007). “Global and local optimization using radial basis function response surface models.” Appl. Math. Modell., 31(10), 2095–2110.
McKay, M. D., Beckman, R. J., and Conover, W. J. (2000). “A comparison of three methods for selecting values of input variables in the analysis of output from a computer code.” Technometrics, 42(1), 55–61.
Mitchell, T. J., and Morris, M. D. (1992). “The spatial correlation function approach to response surface estimation.” Proc., 24th Conf. on Winter Simulation, Association for Computing Machinery, New York.
Palacios, F., et al. (2013). “Stanford university unstructured (SU2): An open-source integrated computational environment for multi-physics simulation and design.” 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, American Institute of Aeronautics and Astronautics, Reston, VA.
Rai, M. M., and Madavan, N. K. (2000). “Aerodynamic design using neural networks.” AIAA J., 38(1), 173–182.
Sederberg, T. W., and Parry, S. R. (1986). “Free-form deformation of solid geometric models.” ACM SIGGRAPH Comput. Graphics, 20(4), 151–160.
Sekishiro, M., Venter, G., and Balabanov, V. (2006). “Combined kriging and gradient-based optimization method.” 11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conf., American Institute of Aeronautics and Astronautics, Reston, VA.
Shyy, W., Papila, N., Vaidyanathan, R., and Tucker, K. (2001). “Global design optimization for aerodynamics and rocket propulsion components.” Prog. Aerosp. Sci., 37(1), 59–118.
Simpson, T., Mistree, F., Korte, J., and Mauery, T. (1998). “Comparison of response surface and kriging models for multidisciplinary design optimization.” 7th AIAA/USAF/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, American Institute of Aeronautics and Astronautics, Reston, VA.
Simpson, T. W., Mauery, T. M., Korte, J., and Mistree, F. (2001). “Kriging models for global approximation in simulation-based multidisciplinary design optimization.” AIAA J., 39(12), 2233–2241.
Song, W., and Keane, A. J. (2007). “Surrogate-based aerodynamic shape optimization of a civil aircraft engine nacelle.” AIAA J., 45(10), 2565–2574.
Spalart, P., and Allmaras, S. (1992). “A one-equation turbulence model for aerodynamic flows.” 30th Aerospace Sciences Meeting and Exhibit, Aerospace Sciences Meetings, American Institute of Aeronautics and Astronautics, Reston, VA.
Vaidyanathan, R., Tucker, K., Papila, N., and Shyy, W. (2004). “CFD based design optimization for a single element rocket injector.” Proc., 41st Aerospace Sciences Meeting and Exhibit, American Institute of Aeronautics and Astronautics, Reston, VA, 296.
Viana, F., and Haftka, R. (2010). “Surrogate-based optimization with parallel simulations using the probability of improvement.” 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conf., American Institute of Aeronautics and Astronautics, Reston, VA.
Wang, J. G., and Liu, G. R. (2002). “On the optimal shape parameters of radial basis functions used for 2D meshless methods.” Comput. Methods Appl. Mech. Eng., 191(23–24), 2611–2630.
Yamazaki, W., and Mavriplis, D. J. (2013). “Derivative-enhanced variable fidelity surrogate modeling for aerodynamic functions.” AIAA J., 51(1), 126–137.
Zhang, Y., and Leithead, W. E. (2005). “Exploiting hessian matrix and trust-region algorithm in hyperparameters estimation of Gaussian process.” Appl. Math. Comput., 171(2), 1264–1281.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 30Issue 6November 2017

History

Received: Aug 3, 2016
Accepted: Mar 29, 2017
Published online: Aug 28, 2017
Published in print: Nov 1, 2017
Discussion open until: Jan 28, 2018

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Authors

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Ph.D. Candidate, National Key Laboratory of Science and Technology on Aerodynamic Design and Research, Northwestern Polytechnical Univ., 127 West Youyi Rd., Xi’an 710072, China. E-mail: [email protected]
Wenping Song [email protected]
Professor, National Key Laboratory of Science and Technology on Aerodynamic Design and Research, Northwestern Polytechnical Univ., 127 West Youyi Rd., Xi’an 710072, China. E-mail: [email protected]
Xudong Yang [email protected]
Professor, National Key Laboratory of Science and Technology on Aerodynamic Design and Research, Northwestern Polytechnical Univ., 127 West Youyi Rd., Xi’an 710072, China (corresponding author). E-mail: [email protected]

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