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Unsteady Drag Measurements for Hypersonic Shock Tunnel

机译:高超音速冲击隧道的非定常阻力测量

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An approach for implementing acceleration compensation in the stress wave force measurement technique was developed by subtracting the inertial force due to acceleration of the model-balance structure from the drag obtained from the SWFM technique. The effective mass of the model-balance structure was approximately constant for a range of calibration impulse magnitudes. However, the acceleration depended on the magnitude. In addition, an integration window was set by a logarithmic decrement technique to account for the impulsive nature of the excitation. Drag obtained with a sphere-cone model mounted in a shock tunnel compared favorably with modified Newtonian values.
机译:通过从SWFM技术获得的阻力中减去由于模型平衡结构的加速度引起的惯性力,开发了一种在应力波力测量技术中实现加速度补偿的方法。对于一系列校准脉冲幅度,模型平衡结构的有效质量近似恒定。但是,加速度取决于大小。另外,通过对数递减技术设置积分窗口以说明激励的脉冲性质。用球形圆锥模型安装在冲击隧道中获得的阻力与修正的牛顿值相比具有优势。

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