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ASSESSMENT OF BODY FORCE METHODOLOGIES FOR THE ANALYSIS OF INTAKE-FAN AERODYNAMIC INTERACTIONS

机译:进气风扇空气动力相互作用分析的体力方法学评估

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With the advent of high bypass ratio turbofan engines of increasing size, new nacelle designs with shorter air intakes have to be considered, creating new aerodynamic interactions with the fan. This paper focuses on a numerical strategy known as Body Force Modeling, in which engine components are modeled and taken into account using source terms in the RANS equation. This approach allows to simulate these interactions with an accuracy comparable to full 360° unsteady simulations, but at a fraction of the cost. Different formulations for the body forces are proposed and applied to different nacelle test cases of varying intake length. Using full annulus unsteady computations as validation data, it is shown that the body force approach allows to capture inlet design effects on in-plane forces and on nacelle flow separation.
机译:随着尺寸越来越大的高旁路比涡轮风扇发动机的出现,必须考虑采用进气量更短的新型机舱设计,从而与风扇产生新的空气动力相互作用。本文着重于一种称为“体力建模”的数值策略,其中使用RANS方程中的源项对发动机组件进行建模并加以考虑。这种方法可以模拟这些相互作用,其精确度可与完整的360°非稳态模拟相媲美,但成本只是其一小部分。提出了不同的机体力公式,并适用于进气长度不同的不同机舱测试用例。使用完整的非定常环空计算作为验证数据,结果表明,体力方法可以捕获入口设计对平面力和机舱流分离的影响。

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