3-D numerical calculation of magnetic drag parachute

被引:0
|
作者
ZHANG ShaoHua [1 ]
ZHAO Hua [2 ]
DU AiMin [1 ]
CAO Xin [1 ]
机构
[1] Key Laboratory of Ionospheric Environment,Institute of Geology and Geophysics,Chinese Academy of Sciences
[2] Center of Spacecraft Assembly Integration and Test,China Academy of Space
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中图分类号
V411 [空气动力学];
学科分类号
摘要
The concept of using an externally applied magnetic field to add the drag force of a hypersonic reentry vehicle during the blackout was proposed by Bush in 1958.The increased drag force is caused by electromagnetic force that is introduced by interaction between the applied magnetic field and the weakly ionized airflow around the reentry vehicle.We investigated the influences of magnetic field intensities on the drag forces of a reentry vehicle by three dimensional(3-D)magnetohydrodynamics(MHD)simulation.The results showed that the drag fore exerted on the vehicle reached 25 kN when the magnetic field was 0.4 T.The drag force increased with the enhanced intial magnetic field.The bow shock was also pushed far away from the vehicle when the magnetic field was strengthened.
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页码:2059 / 2065
页数:7
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