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Effects of pitch, yaw, and roll on delta wing skin friction topology

机译:俯仰,偏航和横滚对三角翼蒙皮摩擦拓扑的影响

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摘要

High-resolution skin friction fields in separated flows over a 65 degrees delta wing and a 76/40 degrees double-delta wing with different junction fillets are obtained by using quantitative global skin friction diagnostics based on luminescent oil visualizations. The topological features such as separation and attachment lines on these delta wings are identified, and the effects of the pitch, yaw, and roll angles on the skin friction topology are studied systematically. The topological consistency of the measured skin friction fields on the delta wings is examined by using the Poincare-Bendixson index formula.
机译:通过使用基于发光油可视化的定量整体皮肤摩擦诊断技术,可以在65度三角翼和76/40度双三角翼上分离流中的高分辨率皮肤摩擦场获得不同的接合角。确定了这些三角翼上的分离和附着线等拓扑特征,并系统地研究了俯仰,偏航和侧倾角对皮肤摩擦拓扑的影响。通过使用Poincare-Bendixson指数公式来检查三角翼上测得的皮肤摩擦场的拓扑一致性。

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