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DIRECT NUMERICAL SIMULATION OF UNSTEADY FINITE-SPAN HYDROFOIL FLOW

机译:非稳态有限跨度水翼流动的直接数值模拟

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The tip-vortex flow over a finite-span hydrofoil with laminar separation on the hydrofoil surface was numerically studied by computing the three-dimensional unsteady Navier-Stokes equations. The computations were direct numerical simulations of all resolvable structures without adding a turbulence model. The topological structure of unsteady separated flow and the influence of the unsteady laminar separated flow on the tip vortex for both swept and unswept hydrofoils were qualitatively investigated. The secondary flow induced by the swept planform played an important role in the unsteadiness of the tip vortex. The interaction between the tip vortex and the unsteady laminar separated flow became stronger as the sweep angle was increased.
机译:通过计算三维非稳态Navier-Stokes方程,数值研究了有限跨度翼型在翼型表面上的层流分离时的涡旋流动。该计算是所有可解析结构的直接数值模拟,而无需添加湍流模型。定性地研究了非恒定分离流的拓扑结构以及非恒定层流分离流对扫掠和未扫掠翼型翼尖涡的影响。掠过的平面型引起的二次流在尖端涡旋的不稳定中起重要作用。随着扫掠角的增加,尖端涡旋与非稳定层流分离流之间的相互作用变得更强。

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