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An Aerodynamic Model for Vane-Type Vortex Generators

机译:叶片式涡流发生器的空气动力学模型

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摘要

A new, physics-based model is presented for flows around vortex generators. The model uses a modified lifting-line method with added physics to account for boundary layer flow. The lifting-line method is extended to also include a vortex lift component and these two components are used to calculate the strength of a vortex shed from an isolated vortex generator. The circulation model is developed further to be used within a CFD framework in a source term approach. Validation is presented, first for the circulation model against a suite of experimental tests for isolated vortex generators where the vortex strength is measured. Excellent agreement is shown that is of the order of the experimental error; 5%. Second, the source term model is validated on a at plate mounted vortex generator problem, and compared to fully-gridded simulations and the commonly used Bender-Anderson-Yagel model. Again, the new method shows excellent agreement, matching well the circulation decay and velocities downstream of the VG.
机译:提出了一种新的基于物理学的模型,用于涡旋发生器周围的流动。该模型使用了改进的提升线方法,并增加了物理特性,以解决边界层流动问题。提升线方法被扩展为还包括涡旋升力分量,并且这两个分量用于计算从隔离涡流发生器产生的涡流脱落的强度。循环模型被进一步开发,以源术语方式在CFD框架内使用。首先介绍了针对循环模型的验证,该验证针对的是一系列测量涡流强度的隔离涡流发生器的实验测试。显示出良好的一致性,接近实验误差; 5%。其次,对源项模型进行了验证,并验证了其与全网格模拟和常用的Bender-Anderson-Yagel模型的比较。再次,新方法显示出极好的一致性,很好地匹配了VG下游的循环衰减和速度。

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