基于CFD 理论的战略大飞机的气动特性数值模拟
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国家自然科学基金资助项目(51375490)


Numerical Simulation of Aerodynamic Characteristics of Large Strategic Aircraft Based on CFD Theory
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    摘要:

    为对概念设计战略大飞机且加装预警雷达天线的气动特性进行对比,采用CATIA 软件,设计一种战略大 飞机的3D 几何模型。基于计算流体力学(computational fluid dynamics,CFD)技术,空气流场的湍流模型采用标准 的k-ε 方程,流体力学控制理论则采用3 维N-S 方程。经Fluent 软件数值模拟,得出战略大飞机的压力系数云图、 速度等值面图和升阻特性,并计算在平飞时飞机的质量和需用推力。结果表明,该研究能对大飞机总体设计提供参 考依据和技术支撑。

    Abstract:

    In order to compare the aerodynamic characteristics of strategic large aircraft and early warning airplane with radar antenna, a 3D model of strategic large aircraft is designed by CATIA software. Based on computational fluid dynamics (CFD) technology, standard k-ε equation is applied to turbulence model of the air flow field, while fluid dynamics control theory adopts the 3D N-S equation. Then numerical simulation of the model is conducted in Fluent software, and the pressure coefficient diagram, velocity contour map and lift-resistance characteristics of the strategic large aircraft are obtained. The weight of the model and required thrust during horizontal flight are also calculated. The results show that the research can provide reference and technical support for the overall design of large aircraft.

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岳奎志.基于CFD 理论的战略大飞机的气动特性数值模拟[J].,2021,40(3).

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  • 收稿日期:2020-11-10
  • 最后修改日期:2020-12-24
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  • 在线发布日期: 2021-03-09
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