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南京航空航天大学 航空学院 飞行器先进设计技术国防重点学科实验室, 江苏 南京 210016
Received:01 March 2022,
Published Online:07 August 2023,
Published:30 July 2023
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Xiaoyuan SUN, Feng DENG, Xueqiang LIU. Numerical Simulation of Ditching of a Twin-Fuselage Aircraft[J]. Acta Armamentarii, 2023, 44(7): 2066-2079.
Xiaoyuan SUN, Feng DENG, Xueqiang LIU. Numerical Simulation of Ditching of a Twin-Fuselage Aircraft[J]. Acta Armamentarii, 2023, 44(7): 2066-2079. DOI: 10.12382/bgxb.2022.0111.
飞机水上迫降过程是一个跨介质过程
即飞机从空气跨越到水的过程。探索和研究物体跨介质过程的物理现象和动态特性
对飞机水上迫降和跨介质飞行器入水砰击等问题具有重要的参考价值。针对某型双机身飞机水上迫降过程展开研究
综合运用URANS(unsteady Reynolds-averaged Navier- Stokes)方法、流体体积模型、动网格技术和6自由度模型对飞机水上迫降过程进行数值模拟。在三维平板水漂运动实验的验证基础上
研究俯仰角度这一关键参数对双机身飞机水上迫降过程的影响。研究结果表明:飞机在水上迫降过程中
俯仰角度越大
飞机的垂向速度峰值越大
垂向位移越大且俯仰偏转角度变化量越小;俯仰角度越小
飞机的水平速度减小得越快
飞机的水平位移越小;飞机以6°俯仰角度水上迫降时受到的水平作用力最大
可以在最短的时间内完成停靠;飞机以14°俯仰角度水上迫降时受到的垂向作用力最大
相同时刻的浸水位移最大。
Aircraft ditching is a trans-media process
namely the process of the aircraft going from air to water. The exploration of the physical phenomena and dynamic characteristics of trans-media objects can provide insights into the research on airplane ditching and water entry of trans-media vehicles. The ditching process of a twin-fuselage aircraft is studied. The unsteady Reynolds-averaged Navier-Stokes (URANS) method
VOF method
dynamic grid technique and 6DOF model are used to numerically simulate the ditching process. Based on the numerical validation of the 3D plate water-skipping experiment
the effect of pitch angle on the ditching process of the twin-fuselage aircraft is analyzed. The numerical results show that: the larger the pitch angle
the greater the peak vertical velocity of the aircraft
the greater the vertical displacement and the smaller the change in pitch deflection angle during the ditching process; the horizontal velocity of the airplane decreases faster and the horizontal displacement of the aircraft is smaller as the pitch angle decreases; when the aircraft ditches with a 6° pitch angle
it is subjected to the largest horizontal force
and therefore stops in the shortest time; when the aircraft ditches with a 14° pitch angle
the vertical force is the largest
and meanwhile the submerged displacement is the largest.
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田北晨 , 刘涛涛 , 吴钦 , 等 . 跨介质飞行器触水滑跳运动特性数值模拟 [J ] . 兵工学报 , 2022 , 43 ( 3 ): 586 - 598 . DOI: 10.12382/bgxb.2021.0164 http://doi.org/10.12382/bgxb.2021.0164 受生活中水漂现象的启发,跨介质飞行器广泛采用灵活机动的滑跳运动模式,大大提高了海战武器的突防能力。基于数值模拟方法研究具有复杂构型的跨介质飞行器触水滑跳运动特性,重点分析入水参数对跨介质飞行器静水面的近水面滑跳运动过程影响。研究结果表明:针对所提跨介质飞行器,近水面滑跳运动可分为稳定滑跳阶段及水面滑行阶段,稳定滑跳阶段飞行器运动轨迹呈类正弦规律波动,逐次入水砰击瞬间飞行器均会受到较大的砰击载荷;跨介质飞行器入水速度v取值为10~55 m/s范围时,随着入水速度增大,可顺利实现近水面滑跳运动的入水俯仰角范围先增大后减小,入水速度为30 m/s时,飞行器入水俯仰角φ有效范围最大为-8°~10°;跨介质飞行器近水面滑跳运动过程中入水速度越大,砰击载荷越大、稳定滑跳次数越多、稳定滑跳距离越远;入水俯仰角φ为0°~5°时飞行器近水面稳定滑跳次数最多,滑跳距离最远,滑跳姿态最稳定。
TIAN B C , LIU T T , WU Q , et al . Numerical simulation on kinematic characteristics of trans-media aircraft during water-skipping [J ] . Acta Armamentarii , 2022 , 43 ( 3 ): 586 - 598 . (in Chinese) DOI: 10.12382/bgxb.2021.0164 http://doi.org/10.12382/bgxb.2021.0164 Inspired by the phenomenon of hydroplaning in life,the flexible skipping motion mode is widely used for trans-media aircraft,which greatly improves the penetration ability of naval weapons. The kinematic characteristics of a trans-media aircraft with complex configuration are studied numerically,and the influence of water-entry parameter on the skipping process of trans-media aircraft over calm water surface is emphatically analyzed. The research results show that the skipping process of trans-media aircraft over water surface can be divided into stable skipping phase and hydroplaning phase,the movement trajectory of trans-media aircraft at the stable skipping phase fluctuates in a sinusoidal pattern,and it is subjected to a large slamming load at every water contact moment. When the water-entry velocity of trans-media aircraft is in the range of 10-55 m/s,the water-entry pitch angle range of the aircraft can increases first and then decreases in the skipping process over water surface with the increase in the entry velocity. When the entry velocity is 30 m/s,the effective range of the water-entry pitch angle of the aircraft is from -8° to 10°.The greater the water-entry velocity is,the greater the slamming load is,the more the number of stable skipping is and the farther the stable skipping distance of the aircraft is. When the pitch angle of water-entry is from 0° to -5°, the trans-media aircraft has the most stable skipping times over the water surface,the longest skipping distance,and the most stable skipping attitude.
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