迎角对导弹初始弹射弹道的影响
Influence of Angle of Attack on Initial Ejection Trajectory of Missile
查看参考文献29篇
|
文摘
|
针对导弹发射的机弹分离过程存在较大不稳定性问题,通过求解流体动力学方程组和刚体六自由度运动方程,仿真分析了迎角对空空导弹初始弹射弹道的影响。参照美国阿诺德工程发展中心开展的一项使用标准机翼/挂架/带舵外挂物模型的捕获轨迹法试验,建立了相似的几何仿真模型并进行了数值计算。通过数值计算结果与文献[29]中风洞试验结果进行对比分析,验证了数值计算方法的可行性;采用该方法计算和分析了四代战机在不同迎角下内埋弹射空空导弹的初始弹道。结果表明:在超声速条件下,迎角变化对导弹初始弹射阶段的六自由度运动有明显的影响;随着迎角的增大,导弹俯仰运动更剧烈、横滚角度更大、偏航角度更小,机弹分离的速度明显下降、分离的安全性逐渐降低。 |
|
其他语种文摘
|
For the instability of separation process of missile, the influence of angle of attack on the initial ejection trajectory of air-to-air missile is analyzed by solving fluid dynamics equations and 6DOF equations of rigid body. Referring to American AEDC's captive trajectory system (CTS) testing, in which uses a generic wing/pylon/finned store model, a similar geometric model is established and numerical calculation is carried out. The feasibility of the numerical calculation method is verified by comparing the numerical results and the CTS results in Ref.[29]. The method is used to calculate and analyze the initial trajectory of an air-to-air missile launched from a fourth-generation fighter under different angles of attack. The following laws are revealed by the analysis: under supersonic condition, 6DOF motion of missile is apparently influenced by the angle of attack at the initial ejection stage. With the increase in the angle of attack, the pitch motion of missile becomes more intense, the roll angle becomes larger, and the yaw angle becomes smaller. The velocity of missile-separation from aiacraft decreases obviously, and the safety of missile-separation from aiacraft decreases gradually. |
|
来源
|
兵工学报
,2021,42(2):438-448 【核心库】
|
|
DOI
|
10.3969/j.issn.1000-1093.2021.02.021
|
|
关键词
|
导弹
;
机弹分离
;
内埋式弹舱
;
动网格
;
弹射弹道
;
迎角
|
|
地址
|
海军航空大学青岛校区, 山东, 青岛, 266041
|
|
语种
|
中文 |
|
文献类型
|
研究性论文 |
|
ISSN
|
1000-1093 |
|
学科
|
武器工业 |
|
文献收藏号
|
CSCD:6938299
|
参考文献 共
29
共2页
|
|
1.
冯金富. 战斗机武器内埋关键技术综述.
飞航导弹,2010(7):71-74
|
CSCD被引
10
次
|
|
|
|
|
2.
常超. 内埋弹射武器机弹安全分离技术综述.
现代防御技术,2012,40(5):67-74
|
CSCD被引
7
次
|
|
|
|
|
3.
刘乐卿. F/A-22隐身战机武器投放仿真与试验技术.
兵器装备工程学报,2016,37(10):8-12
|
CSCD被引
3
次
|
|
|
|
|
4.
Lijewski L E. Time-accurate computational fluid dynamics approach to transonic store separation trajectory prediction.
Journal of Aircraft,1994,31(4):886-891
|
CSCD被引
17
次
|
|
|
|
|
5.
Prewitt N C. Parallel computing of overset grids for aerodynamic problems with moving objects.
Progress in Aerospace Sciences,2000,36(2):117-172
|
CSCD被引
17
次
|
|
|
|
|
6.
Snyder D. Transonic store separation using unstructured CFD with dynamic meshing.
Proceedings of the 33rd AIAA Fluid Dynamics Conference And Exhibit,2003:3919
|
CSCD被引
1
次
|
|
|
|
|
7.
Koomullil R. Moving-body simulations using overset framework with rigid body dynamics.
Mathematics & Computers in Simulation,2008,78(5/6):618-626
|
CSCD被引
4
次
|
|
|
|
|
8.
Prewitt N C. Multiple-body trajectory calculations using the Beggar Code.
Journal of Aircraft,2012,36(5):802-808
|
CSCD被引
3
次
|
|
|
|
|
9.
Osman A A. Numerical analysis of an external store separation from an airplane.
Proceedings of AIAA Modeling and Simulation Technologies Conference,2016:2143
|
CSCD被引
1
次
|
|
|
|
|
10.
Baysal O. Interference flows past cylinder-fin-sting-cavity assemblies.
Journal of Aircraft,1992,29(2):194-202
|
CSCD被引
1
次
|
|
|
|
|
11.
Fouladi K. Viscous simulation method for unsteady flows past multicomponent configurations.
Journal of Fluids Engineering,1992,114(2):161-169
|
CSCD被引
1
次
|
|
|
|
|
12.
Lawson S J. Review of numerical simulations for high-speed, turbulent cavity flows.
Progress in Aerospace Sciences,2011,47(3):186-216
|
CSCD被引
39
次
|
|
|
|
|
13.
Anandhanarayanan K. Se-paration dynamics of air-to-air missile using a grid-free Euler solver.
Journal of Aircraft,2013,50(3):725-731
|
CSCD被引
6
次
|
|
|
|
|
14.
Johnson M W. A novel Cartesian CFD cut cell approach.
Computers & Fluids,2013,79:105-119
|
CSCD被引
2
次
|
|
|
|
|
15.
Merrick J D.
Influence of Mach number and dynamic pressure on cavity tones and freedrop trajectories. Wright-Patterson AFB, OH,2014
|
CSCD被引
1
次
|
|
|
|
|
16.
沈琼. 无人机机载导弹分离轨迹的数值仿真.
弹箭与制导学报,2009,29(5):99-102
|
CSCD被引
2
次
|
|
|
|
|
17.
李杰. 不同释放力组合下小型外挂物投放的数值模拟.
北京理工大学学报,2010,30(3):23-26
|
CSCD被引
1
次
|
|
|
|
|
18.
段旭鹏. 基于动态混合网格的多体分离数值模拟方法.
空气动力学学报,2011,29(4):447-452
|
CSCD被引
15
次
|
|
|
|
|
19.
唐上钦. 考虑气动干扰的导弹内埋式发射弹道研究.
弹箭与制导学报,2013,33(3):138-142
|
CSCD被引
12
次
|
|
|
|
|
20.
曾铮. RBF 整体网格变形技术与多体轨迹仿真.
空气动力学学报,2015,33(2):170-177
|
CSCD被引
10
次
|
|
|
|
|
了解气象卫星更多信息，请访问