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Influence of Penetration Deflection by the Shape of Tail Oblique Cone of Projectile
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Dingshan ZHANG1, Bo ZHANG1, Liang FU2, Xiao XU1, Pengfei LI1
Chinese Journal of High Pressure Physics | 2024, 38(1) : 015101-1 - 015101-10
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Chinese Journal of High Pressure Physics | 2024, 38(1): 015101-1-015101-10
• High Pressure Applications •
Influence of Penetration Deflection by the Shape of Tail Oblique Cone of Projectile
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Dingshan ZHANG1, Bo ZHANG1, Liang FU2, Xiao XU1, Pengfei LI1
Affiliations
  • 1Xi’an Modern Chemistry Research Institute, Xi’an 710065, Shaanxi, China
  • 2Norinco Group Testing and Research Institute, Huayin 714200, Shaanxi, China
Published: 2024-02-05 doi: 10.11858/gywlxb.20230728
Outline
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Aiming at the problem of deflection when the projectile obliquely penetrates a multi-layer target, a theoretical calculation model of the projectile deflection caused by the oblique cone structure of the projectile tail is established, and the change rule of the deflection with the tail structure is obtained at the working conditions of the velocity of 0.2−1.2 km/s, the angle of attraction of −30°−20°, the radius of the projectile body of 30–60 mm, and the angle between bevel plane of tail and the projectile shaft of 0°−4°. Moreover, the accuracy of the model is verified by comparing with the test results. The results showed that the tail of the projectile forms a negative deflection moment and the projectile produces a “head down” effect when the tail of the projectile penetrated upward target, and the tail of the projectile forms a positive deflection moment and the projectile produces a “head up” effect when the tail of the projectile penetrated downward target; the deflection moment of vertical axis is about 100 times greater than that of parallel axis. The deflecting moment can be increased by increasing the angle between bevel plane of tail and the projectile shaft, the length of the tail, and the radius of the projectile. Increasing the angle between bevel plane of tail and the projectile shaft is more effective in increasing the deflection moment than increasing the tail length.

multi-layer target  /  penetration  /  deflection moment  /  tail shape  /  oblique cone structure
张丁山, 张博, 付良, 徐笑, 李鹏飞. 弹体尾部斜锥面形状对侵彻偏转的影响. 高压物理学报, 2024 , 38 (1) : 015101-1 -015101-10 . DOI: 10.11858/gywlxb.20230728
Dingshan ZHANG, Bo ZHANG, Liang FU, Xiao XU, Pengfei LI. Influence of Penetration Deflection by the Shape of Tail Oblique Cone of Projectile[J]. Chinese Journal of High Pressure Physics, 2024 , 38 (1) : 015101-1 -015101-10 . DOI: 10.11858/gywlxb.20230728
Year 2024 volume 38 Issue 1
13
6
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Article Info
doi: 10.11858/gywlxb.20230728
  • Receive Date:2023-08-28
  • Online Date:2026-11-05
  • Published:2024-02-05
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History
  • Received:2023-08-28
  • Revised:2023-11-21
Affiliations
    1Xi’an Modern Chemistry Research Institute, Xi’an 710065, Shaanxi, China
    2Norinco Group Testing and Research Institute, Huayin 714200, Shaanxi, China
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表12种不同金属材料的力学参数
科
Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)
属
Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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