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- W2365222265 abstract "The unique aim of aerodynamic designer is always to enhance lift coefficient and reduce drag coefficient.Wing aerodynamic design is the core of aircraft aerodynamic design and controlling transition between the wing section is one of the effective measures to enhance lift coefficient and reduce drag coefficient.The article firstly analyzes the aerodynamic characteristic of state in detail that there are no constraint between the two sections at the root of the wing.According to result that is not very well,new plans and ideas are established.The aerodynamic performance of two other types between the two section is studied when the section of the wing is unchanged.How to improve the aerodynamic performance in terms of transition styles is learned.Finally,three distinguished results are compared and the preliminary regular pattern of the transition between the sections at the root of wing is achieved.The result demonstrates that it gets satisfactory results when using transition of raised curve and linear line.The wing using the transition of raised curve improves the aerodynamic performance,the drag coefficient of the wing drop 5*10.Linear transition also enhances aerodynamic performance eliminates the shock wave and can meet the target of designation better." @default.
- W2365222265 created "2016-06-24" @default.
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- W2365222265 date "2010-01-01" @default.
- W2365222265 modified "2023-09-23" @default.
- W2365222265 title "Research on Aerodynamic Performance Impact on Modeling Surfaces of Wing" @default.
- W2365222265 hasPublicationYear "2010" @default.
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