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Integrated analysis of aerodynamic/stealth characteristics of blended-wing-body lifting vehicle

机译:混纺机翼体升降车的空气动力学/隐形特性综合分析

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In this paper, a blended-wing-body lifting vehicle is designed, with the cross section described by Class/Shape transformation method (CST), the outline controlled by an exponential function, and tail regulated by B-spline curve. Rapid estimation procedures of aerodynamic based on plane method and of radar cross section (RCS) based on physical optics are developed and validated. A frame of integrated design and analysis of aerodynamic and stealth characteristics is constructed and applied to parameter sensitivity analysis. The results show that the parameters that affect the aerodynamic differ from those of RCS, which means the vehicle could be good at both aerodynamic and stealth, and the study followed should be focused on it.
机译:在本文中,设计了混合 - 翼体升降车辆,具有由类/形状变换方法(CST)描述的横截面,由指数函数控制的轮廓和由B样条曲线调节的尾部。基于平面方法和基于物理光学的雷达横截面(RCS)的快速估计程序,并验证了基于物理光学器件的雷达横截面(RCS)。构建和应用空气动力学和隐形特性的集成设计和分析框架,并应用于参数敏感性分析。结果表明,影响空气动力学的参数与RCS的参数不同,这意味着车辆可以擅长空气动力学和隐形,并且该研究尤为关注它。

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