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Time-dependent airloads on a cylinder in a supersonic cavity

机译:超声腔中气缸上随时间变化的空气载荷

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Normal force and pitching moment is experimentally obtained on a slender cylinder at two different angles of attack at several static positions and translating motions from within a cavity to outside Mach 1.5 freestream. Measurements reveal a constant normal force and pitching moment within the cavity at 0° and large variations throught the shear layer to the outside freestream. At 5° angle of attack, force and pitching moment has constant positive gradient from the cavity ceiling to the shear layer. Frequency spectra is relatively well predicted by Rossiter's second- and third modes, and overall high-content frequencies translated slightly to lower frequencies. Dynamic motions has good repeatability and exhibit a different unsteady force and moment trajectory from quasi-steady, even at a motion as slow as 1790 convective times.
机译:法向力和俯仰力矩是通过在细长圆柱体上以两个不同的迎角在几个静态位置处获得的,并将运动从腔体内转换为1.5马赫外自由流而获得的。测量结果表明,腔体内部在0°处具有恒定的法向力和俯仰力矩,并且在剪切层与外部自由流之间存在较大的变化。在攻角为5°时,力和俯仰力矩从型腔顶部到剪力层具有恒定的正梯度。 Rossiter的第二和第三模式可以相对较好地预测频谱,并且将高含量的总频率稍微转换为较低的频率。动态运动具有良好的重复性,并且即使在慢至1790对流时间的情况下,也表现出与准稳态不同的不稳定力和力矩轨迹。

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