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- W2349620777 abstract "The joined-wing,characterized by low structural weight,small induced drag,big lift coefficient and good stability,is different from normal layout.Five design variables which have significant effect on the joined-wing are selected,and influence on the aerodynamic performance of joined-wing is analyzed by numerical simulation in this paper.Moreover,response surface methodology is applied to improve optimization efficiency,and simulated annealing algorithm is used to solve objective functions in optimization design.The results show that increasing average aerodynamic chord length of front and aft wing and space between them,with V-type decal age and invariable wing area,could reduce the interference and increase lift-drag ratio effectively." @default.
- W2349620777 created "2016-06-24" @default.
- W2349620777 creator A5082924617 @default.
- W2349620777 date "2010-01-01" @default.
- W2349620777 modified "2023-09-23" @default.
- W2349620777 title "Aerodynamic design and optimization for joined wing based on Response Surface Methodology" @default.
- W2349620777 hasPublicationYear "2010" @default.
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