1.
Research on Super-Sonic Missile Guidance Plan Based on the Terminal Angular Constraint
基于落角约束的超声速导弹制导方案研究
2.
Engineering Calculation Method for Supersonic Missile's Axial Force in Large-Scale Attack/Deflection Angle
大攻角/舵偏角条件下超声速导弹轴向力工程计算方法
3.
Study of Inlets/body Aerodynamic Interference of Supersonic Tactical Missile Using Numerical Simulation;
超声速战术导弹进气道/弹身气动干扰数值研究
4.
Method Research on Trajectory Design and Optimization of Hypersonic Cruise Missile;
高超声速巡航导弹弹道设计与优化方法研究
5.
Forecast Variable Structure Midcourse Guidance Law Design for Supersonic Intercept Missile
超声速拦射导弹的一种预测变结构中制导律
6.
Experimental investigation on pressure distribution characteristics of wings of ×× missile at supersonic speeds and high angles of attack
××导弹翼面超声速大迎角压力分布特性试验研究
7.
Combat Effectiveness Analyses of Air-launched Hypervelocity Cruise Missile to Surface;
空射高超声速巡航导弹对地作战效能分析
8.
Research of supersonic cruise missile and ramjet motor integration based on energy method
基于能量法的超声速飞航导弹/冲压发动机一体化研究
9.
Calculous Pyonephrosis Treated by Percutaneous Nephrolithotomy with a Combination Pneumatic and Ultrasonic Lithotripsy under the Guidance of Ultrasonography
超声引导经皮肾镜弹道超声治疗结石性脓肾
10.
Numerical Study of Pitching Dynamic Characteristic for Hypersonic Missile
高超声速弹头俯仰动态特性数值研究
11.
Aerodynamics and Aerodynamic Heating Research for the Wing of Hypersonic Projectile;
高超声速弹箭尾翼（弹翼）的气动力与气动热研究
12.
Thermal-structural coupling analysis on wing short-range hypersonic missile
近程高超音速导弹弹翼热结构耦合分析
13.
Investigation on Design of Altitude Control System of the Missile with Supersonic Speed at Minimum Altitude;
超音速超低空导弹高度控制系统设计与研究
14.
High-velocity Long-distance Surface-to-surface Missile Infrared Image Seeker
超高速远程地地导弹红外凝视成像导引头设计
15.
An example for hypersonic blunted cone flow in ballistic range is illustrated.
示例给出了弹道靶中高超声速钝锥流动的应用
16.
The Aerodynamic Ablation of Hypersonic Penetrator Shell at Angle of Attack
有攻角高超声速穿甲弹气动烧蚀的研究
17.
Aerodynamic Heating and Electron Distribution Research on Hypersonic Warhead
高超声速弹头气动热及电子分布的研究
18.
Numerical Solution of Optimal Trajectory for Hypersonic Vehicle with Constraints
带约束的高超声速飞行器最优弹道的数值算法