An improved adaptive sampling and experiment design method for aerodynamic optimization

Abstract Experiment design method is a key to construct a highly reliable surrogate model for numerical optimization in large-scale project. Within the method, the experimental design criterion directly affects the accuracy of the surrogate model and the optimization efficient. According to the shortcomings of the traditional experimental design, an improved adaptive sampling method is proposed in this paper. The surrogate model is firstly constructed by basic sparse samples. Then the supplementary sampling position is detected according to the specified criteria, which introduces the energy function and curvature sampling criteria based on radial basis function (RBF) network. Sampling detection criteria considers both the uniformity of sample distribution and the description of hypersurface curvature so as to significantly improve the prediction accuracy of the surrogate model with much less samples. For the surrogate model constructed with sparse samples, the sample uniformity is an important factor to the interpolation accuracy in the initial stage of adaptive sampling and surrogate model training. Along with the improvement of uniformity, the curvature description of objective function surface gradually becomes more important. In consideration of these issues, crowdness enhance function and root mean square error (RMSE) feedback function are introduced in C criterion expression. Thus, a new sampling method called RMSE and crowdness enhance (RCE) adaptive sampling is established. The validity of RCE adaptive sampling method is studied through typical test function firstly and then the airfoil/wing aerodynamic optimization design problem, which has high-dimensional design space. The results show that RCE adaptive sampling method not only reduces the requirement for the number of samples, but also effectively improves the prediction accuracy of the surrogate model, which has a broad prospects for applications.

[1]  F. Menter Two-equation eddy-viscosity turbulence models for engineering applications , 1994 .

[2]  Zhao Ke Airfoil optimization based on distributed particle swarm algorithm , 2011 .

[3]  Gregory E. Fasshauer,et al.  Meshfree Approximation Methods with Matlab , 2007, Interdisciplinary Mathematical Sciences.

[4]  Robert E. Smith,et al.  Transfinite Interpolation (TFI) Generation Systems , 1999 .

[5]  Christian B Allen,et al.  Comparison of Adaptive Sampling Methods for Generation of Surrogate Aerodynamic Models , 2013 .

[6]  Wenbo Xu,et al.  Particle swarm optimization with particles having quantum behavior , 2004, Proceedings of the 2004 Congress on Evolutionary Computation (IEEE Cat. No.04TH8753).

[7]  J. Samareh Aerodynamic Shape Optimization Based on Free-form Deformation , 2004 .

[8]  Zhao Ke,et al.  Robust Design of Supercritical Wing Aerodynamic Optimization Considering Fuselage Interfering , 2010 .

[9]  James Kennedy,et al.  Particle swarm optimization , 2002, Proceedings of ICNN'95 - International Conference on Neural Networks.

[10]  Marco Ceze,et al.  A Study of the CST Parameterization Characteristics , 2009 .

[11]  Reinhard Radermacher,et al.  Cross-Validation Based Single Response Adaptive Design of Experiments for Deterministic Computer Simulations , 2008 .

[12]  Paul G. A. Cizmas,et al.  Mesh Generation and Deformation Algorithm for Aeroelasticity Simulations , 2007 .

[13]  Martin D. Buhmann,et al.  Radial Basis Functions , 2021, Encyclopedia of Mathematical Geosciences.

[14]  Xu Fang Study of Robust Winglet Design Based on Arbitrary Space Shape FFD Technique , 2013 .

[15]  S. Jakobsson,et al.  Rational radial basis function interpolation with applications to antenna design , 2009, J. Comput. Appl. Math..

[16]  Brenda Kulfan,et al.  Recent extensions and applications of the ‘CST’ universal parametric geometry representation method , 2010, The Aeronautical Journal (1968).

[17]  S. P. Spekreijse,et al.  An algorithm to check the topological validaty of multi-block domain decompositions , 1998 .

[18]  Arno Ronzheimer Post-Parametrization of CAD-Geometries Using Freeform Deformation and Grid Generation Techniques , 2004 .

[19]  B. Kulfan A Universal Parametric Geometry Representation Method - "CST" , 2007 .

[20]  E. Toro,et al.  Restoration of the contact surface in the HLL-Riemann solver , 1994 .