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关于前掠翼诱导阻力特性的分析

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前掠翼是飞行器布局的形式之一,关于前掠翼诱导阻力气动特性问题,已有的文献中给出了让人产生混淆的认识.为了澄清关于前掠翼诱导阻力问题的概念,分别采用非线性升力面、升力线和高精度求解欧拉方程的方法计算和分析前掠翼诱导阻力特性,与对应的后掠翼、直机翼进行对比,并对前掠翼的优点进行简要梳理.结果表明:前掠翼诱导阻力比后掠翼小的认知是存在问题的,即使在势流理论的框架下,前掠翼的诱导阻力也比后掠翼大.
Analysis on induced drag characteristics of forward swept wings
Forward swept wing is one of the plane forms of aircraft configuaration.For aerodynamic characteristics of induced drag of forward swept wings,the existing papers have provided confusing understandings.In order to clarify the mechanism of induced drag of forward swept wings,the induced drag characteristics are calculated and analyzed for different wing plane forms.The forward swept wings,aft-swept wings and straight wings are consid-ered and compared with nonlinear vortex lattice method,lifting-line theory,and high-order Euler equations nu-merical methods.The advantages of forward swept wings are also briefly summarized.The results show that con-ventional perception that the induced drag of forward swept wings is smaller than that of aft-swept wings is a misun-derstanding.Even within the framework of potential flow theory and based on numerical results with Navier-Stokes equations,the induced drag of forward swept wings is greater than that of aft-swept wings.

forward swept winginduced dragpotential flow theorylift surface theorynumerical simulation

叶正寅、周欣欣、叶赋晨

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西北工业大学 航空学院,西安 710072

飞行器基础布局全国重点实验室,西安 710072

中国航天空气动力研究院,北京 100086

前掠翼 诱导阻力 势流理论 升力面理论 数值模拟

2024

航空工程进展
中国航空学会 西北工业大学

航空工程进展

CSTPCD
影响因子:0.207
ISSN:1674-8190
年,卷(期):2024.15(6)