工程约束下基于自由曲面方法的机头气动修形设计

Aerodynamic design of forward fuselage using NURBS with engineering constraints

  • 摘要: 二次曲线由于其良好的几何特征,在传统的飞机建模过程中得到较多的应用,但是单一的控制参数使其外形变化受到限制,而灵活的外形变化恰是NURBS曲线的主要特点。根据飞机设计过程中总体布局要求及人机工效约束条件,采用NURBS曲线曲面方法,使用控制点位置的相对长度与角度为设计参数,在飞机机头参数化建模过程中融入相关的工程约束,通过CFD计算分析,对设计参数进行优化,得到符合要求的模型;并尝试在风挡区域增加一条横向控制线,调节风挡局部区域的气流流动。结果表明,采用NURBS方法可以得到符合设计要求的机头外形,而且对外形的控制更加灵活;增加风挡区域的横向控制线改善了风挡局部区域的气流流动。

     

    Abstract: CFD method has the advantage of well simulating the flow over wind farm of complex terrain,compared with the method of using the software WAsP with linear model, thus becoming the development direction of assessment of wind resources in complex terrain. In order to use the CFD package FINE/TURBO and standard k-ε turbulence model with wall function in the wind resources assessment and micrositing of wind farm in the complex terrain, in this paper, Island Nanao had been simulated in wind directions at intervals of 30 degrees,under the assumption of neutral condition, to investigate the influence of inlet condition on the results. The simulation results show that the wind speed-up and intensity don't change essentially under different inlet conditions. Based on this law, with whole year wind data, an assessment method with post processing has been built, providing a strong reference for engineering practice.

     

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