28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION DESIGN OF MULTI-ELEMENT AIRFOIL USING KRIGING MODEL
R. F. Xu, R. Z. Qian, W. Lei
AVIC, The First Aircraft Inst., Xi'an, China
Keywords: kriging model, multi-element airfoil, optimization design
In this paper, multi-objective aerodynamic design of the multi-element airfoil based on Kriging model is carried out. For flow analysis, a 2-D N-S solver using zonal patched grids which produced automatically and efficiently is applied. Utilizing the above method, the aerodynamic characteristic of the airfoil is greatly improved.
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