微气泡致动器技术在弹丸飞行中的应用
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Application of Micro Bubble Actuator Technology in Projectile Flight
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    摘要:

    为研究不同的气泡高度对弹丸的影响,建立带有不同高度微气泡致动器弹丸的模型,对不同弹丸进行气 动仿真,分析带有不同高度的微气泡致动器对弹丸阻力系数所产生的影响,并计算出全弹道的飞行过程。仿真结果 表明:加装不同高度的微气泡对弹丸的飞行稳定性影响很小;相同马赫数、相同攻角情况下带有气泡致动器的弹丸 阻力系数小于普通弹丸,升力系数大于普通弹丸,能够有效地增大射程和减小横向偏移。

    Abstract:

    In order to study the effect of different bubble heights on the projectile, the model of micro bubble actuators with different heights is established, and the aerodynamic simulation of different projectile is carried out, the influence of micro bubble actuators with different heights on the projectile resistance coefficient is analyzed, and the flight process of the full trajectory is calculated. The simulation results show that adding micro-bubbles of different heights has little effect on the flight stability of the projectile. At the same Mach number and angle of attack, the drag coefficient of the projectile with bubble actuator is lower than that of an ordinary projectile, and a lift coefficient higher than that of an ordinary projectile, which can effectively increase the range and reduce the lateral deviation.

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引用本文

邱海峰.微气泡致动器技术在弹丸飞行中的应用[J].,2020,39(04).

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  • 收稿日期:2019-12-05
  • 最后修改日期:2020-01-11
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  • 在线发布日期: 2020-05-06
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