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On the shape and motion of the Earth's bow shock

机译:关于地球弓激波的形状和运动

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摘要

Multipoint-measurements by the magnetic field Cluster-FGM (Flux Gate Magnetometer) are used to determine the local shock normal, and in turn allow the study of shock location shape and the velocity of the Earth's bow shock. The shock crossings cover orbits in which the spacecraft separation is of the order of ~600 km or less. A data selection of 133 bow shock crossings, ranging from quasi-steady perpendicular to moderately noisy oblique geometries, have been analyzed using a standard timing analysis. Prior to applying the timing technique, the magnetic field fluctuations, when present, are suppressed using low band-pass filtering. The present study contributes to similar studies conducted in the past and available in the literature through the inclusion of a larger data set. The shock standoff distance is determined conjointly with a paraboloid model and the results from a timing analysis. A statistical study reveals a standoff distance well in agreement with the standard gas dynamics model prediction for high Mach number M_A. We have also found that for about half the crossings, the timing shock normals agree, within 11°, with a conic-based shock model. Our results strongly indicate that the motion of the shock is predominantly along the Sun-Earth direction; a departure from this direction is not related to the shock-crossing location. Shock velocities below ~ 80 km/s satisfactorily follow a nearly Gaussian distribution with zero mean and a standard deviation of ~ 42 km/s. Finally, we show that high speed motions are correlated with sharp increases in the solar wind upstream ram pressure, and are consistent with gas dynamics model predictions.
机译:使用磁场簇FGM(磁通门磁力计)进行多点测量来确定局部冲击法线,进而可以研究冲击位置形状和地球弓形冲击的速度。冲击波横穿的轨道中,航天器的间隔约为600 km或更小。已使用标准时序分析对133个弓形激波穿越的数据选择进行了分析,范围从准稳态垂直到中等噪声的倾斜几何形状。在应用定时技术之前,使用低带通滤波可抑制磁场波动(如果存在)。本研究为过去进行的类似研究做出了贡献,并且通过包含更大的数据集可从文献中获得。通过抛物面模型和时序分析的结果共同确定冲击距离。一项统计研究表明,与高马赫数M_A的标准气体动力学模型预测相吻合的井距距离很好。我们还发现,对于大约一半的交叉路口,正时冲击法线与基于圆锥曲线的冲击模型在11°内一致。我们的结果强烈表明,震动的运动主要是沿着太阳地球的方向进行的。与该方向的偏离与避震位置无关。低于80 km / s的冲击速度令人满意地遵循接近高斯的分布,均值为零,标准差为42 km / s。最后,我们证明了高速运动与太阳风上游闸板压力的急剧增加相关,并且与气体动力学模型的预测一致。

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