A dynamic response simulation of aluminum plate target induced by high-altitude nuclear detonation X-ray

YU Runzhou; ZHANG Kun; TANG Wenhui

doi:10.11883/bzycj-2024-0082

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YU Runzhou, ZHANG Kun, TANG Wenhui. A dynamic response simulation of aluminum plate target induced by high-altitude nuclear detonation X-ray[J]. Explosion And Shock Waves. doi: 10.11883/bzycj-2024-0082

Citation:

YU Runzhou, ZHANG Kun, TANG Wenhui. A dynamic response simulation of aluminum plate target induced by high-altitude nuclear detonation X-ray[J]. Explosion And Shock Waves. doi: 10.11883/bzycj-2024-0082

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A dynamic response simulation of aluminum plate target induced by high-altitude nuclear detonation X-ray

doi: 10.11883/bzycj-2024-0082

College of Science, National University of Defense Technology, Changsha 410073, Hunan, China

Received Date: 2024-03-27
Rev Recd Date: 2024-05-30

Available Online: 2024-05-30

Abstract

Abstract

When X-rays generated by high-altitude nuclear detonation irradiates on the shell structure of missile, blow-off impulse (BOI) and thermal shock waves generated may produce dynamic response and damage on it. The existing three one-dimensional theoretical models, Whitener, BBAY, and MBBAY, can only provide approximate BOI values and accurate results of peak pressure and other information are inaccessible. Solving this problem requires numerical calculations based on real physical laws. The numerical simulation program TSHOCK3D for X-ray thermal excitation wave is used to calculate the BOI and peak pressure to make a comparative analysis. An aluminum plate with a length and width of 0.4 centimeters and a thickness of 0.1 centimeters is set as the target for X-ray radiation. The range of the working conditions is 0.1−3.0 keV for the Planck's blackbody temperatures and radiant energy flux are in the range of 220−400 J/cm². The results indicate that the TSHOCK3D can give the results effectively and reliably. The simulation results are consistent with the theoretical models mentioned above. The BOI and peak pressure are approximately linear with the energy flux, while the maximum value exist for different blackbody temperatures.
- X-ray,
- blow-off impulse,
- thermal shock wave,
- TSHOCK3D

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References(22)

References

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