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Comparison of Numerical and Experimental Data in the Wake of Combat Aircraft Airbrakes

机译:作战飞机空气吹风机中数值和实验数据的比较

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摘要

In the course of an airbrake design study DES simulations and wind tunnel tests of a limited set of airbrake shapes have been performed. The principal suitability of DES simulations in this design task is briefly shown. In the wind tunnel tests particle image velocimetry measurements have been used for determining the mean values and turbulent fluctuations of the velocity field. Those quantities are compared to the numerical results in order to assess the accuracy of the numerical simulation. Measurements have been made in the symmetry plane as well as in two horizontal planes. In one of these horizontal planes focused measurements of the shear layer development near the airbrake edge were performed.
机译:在空气制动器设计的过程中,已经进行了DES模拟和风洞测试有限一组空气煞白。简要展示了该设计任务中DES模拟的主要适用性。在风洞中,测试粒子图像测速仪已经用于确定速度场的平均值和湍流波动。将这些数量与数值结果进行比较,以评估数值模拟的准确性。在对称平面以及两个水平平面中进行了测量。在这些水平面之一中,进行了剪切层开发的聚焦测量,避风机边缘附近的剪切层显影。

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