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Study of Vortex Breakdown and Pitch up on a Compound Delta Wing

机译:复合三角翼的涡旋破坏与俯仰研究

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This paper discusses the calculation of mean pressure on a compound delta wing configuration and its variance to understand vortex breakdown and pitch up on the setup. The configuration of the compound delta wing being used was 50°-60°. The data was used to find the location of vortex breakdown and pitch up over the compound delta wing. It was done using calibration of different pressure ports on span and chord wise location of the wing. The pressure values were then converted to Coefficient of Pressure (Cp) for proper study and comparison.
机译:本文讨论了复式三角翼构型的平均压力的计算及其方差,以了解旋涡的破裂和在装置上的俯仰。使用的复合三角翼的构型为50°-60°。该数据用于查找涡旋破裂和复合三角翼上方俯仰的位置。使用机翼跨度和弦向位置上不同压力端口的校准来完成。然后将压力值转换为压力系数(Cp),以进行适当的研究和比较。

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