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Aerodynamic Characteristics of Tail Wing of Non-lethal Long-range Low-velocity Electric Shock Bullet
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Xu LI, Yao-hui CHEN*, Dao-ping ZHANG, Zhi-fei LUO
Science Technology and Engineering | 2025, 25(13) : 5422 - 5428
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Science Technology and Engineering | 2025, 25(13): 5422-5428
Papers·Weapon Technology
Aerodynamic Characteristics of Tail Wing of Non-lethal Long-range Low-velocity Electric Shock Bullet
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Xu LI, Yao-hui CHEN*, Dao-ping ZHANG, Zhi-fei LUO
Affiliations
  • National Key Laboratory of Transient Physics, Nanjing University of Science and Technology, Nanjing 210094, China
Published: 2025-05-08 doi: 10.12404/j.issn.1671-1815.2404461
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The non-lethal electric shock weapon is a research hotspot in the field of non-lethal weapons. In recent years, the research on wireless long-range electric shock bullets has become a key issue within this field. Therefore, aiming at the design of non-lethal long-range low-velocity electric shock bullet empennage, three airfoils of Clark Y, Eppler 387 and NACA-66 with good aerodynamic characteristics at low velocity were selected. The simulation results of NACA0012 airfoil at 30 m/s using CFD software were compared with the literature simulation results and wind tunnel test results to verify the algorithm's effectiveness. Subsequently, the aerodynamic characteristics of the three airfoils at low velocity were simulated, and the lift coefficient, drag coefficient and lift-drag ratio corresponding to different angles of attack at 30, 35 and 40 m/s were obtained respectively. The results show that at the same flight velocity, the lift coefficient and drag coefficient of the three airfoils gradually increase with the increase of the angle of attack, but the growth rate of the lift coefficient gradually decreases, and the growth rate of the drag coefficient gradually increases. The lift-to-drag ratio increases first and then decreases with the increase of the angle of attack. After comparison, it is found that the aerodynamic performance of the airfoil Eppler 387 is better than that of the other two airfoils. The velocity of 40 m/s and the angle of attack between 4° and 6° are the best working conditions, which can not only meet the structural design requirements of non-lethal long-range low-velocity electric shock bullets, but also produce less drag while providing as much rolling moment as possible.

long-range electric shock weapon  /  non-lethal  /  low-velocity airfoil  /  aerodynamic characteristics  /  numerical simulation
Xu LI, Yao-hui CHEN, Dao-ping ZHANG, Zhi-fei LUO. Aerodynamic Characteristics of Tail Wing of Non-lethal Long-range Low-velocity Electric Shock Bullet[J]. Science Technology and Engineering, 2025 , 25 (13) : 5422 -5428 . DOI: 10.12404/j.issn.1671-1815.2404461
Year 2025 volume 25 Issue 13
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doi: 10.12404/j.issn.1671-1815.2404461
  • Receive Date:2024-06-14
  • Online Date:2025-07-09
  • Published:2025-05-08
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  • Received:2024-06-14
  • Revised:2025-01-22
Affiliations
    National Key Laboratory of Transient Physics, Nanjing University of Science and Technology, Nanjing 210094, China
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

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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