DAN WAKE LATIN HYPERCUBE SAMPLING SKU SERIES

Under Variable Operation Conditions Based on LI Qianglin, ZENG Weijie, TIAN Zhen, GU Bo.ДЄdaptability of Multi-Structure of Finned Tube Heat Exchanger Journal of Shanghai Jiaotong University, 2020, 54(9): 916-923.ДЄdaptive Control of Non-Affine Pure Feedback Nonlinear Switching Systems Optimal Control of Effluent Ammonia Nitrogen for Municipal Wastewater Treatment Process HAN Honggui, YANG Shiheng, ZHANG Lu, QIAO Junfei.

The combined optimization method evidently improves the efficiency of the airfoil aerodynamic optimization procedure.ДЄdaptive NN-SM Control for Path Following of Underactuated Surface Vessels The results show that the modified Hicks-Henne shape function describes the airfoil leading edge with satisfaction. The lift to drag ratio optimization design of NACA 0006 was performed as an example using this combined strategy. Finally, the optimization of the objective function using the multiоЂ‘island genetic algorithm(MIGA) based on the neural network approximation model was performed to achieve the optimal results. Subsequently, those simulated data sets were used to train the RBF neural network.

DAN WAKE LATIN HYPERCUBE SAMPLING SKU SERIES

Then, Latin hypercube sampling was applied to generate the samples, whose aerodynamic performances were obtained from a series of CFD simulations. First, a modified method of original Hicks-Henne shape function was adopted to parametrically describe the leading edge. Aimed to gain a high aerodynamic efficiency in various flight conditions, the aerodynamic optimization of the adaptive airfoil leading edge was conducted based on Isight platform.

Dan wake latin hypercube sampling sku