说明:双击或选中下面任意单词,将显示该词的音标、读音、翻译等;选中中文或多个词,将显示翻译。
您的位置:首页 -> 句库 -> 气动外形设计
1.
Design of Aerodynamic Configuration of SS8 Quasi-high Speed Electric Locomotive
韶山8型准高速电力机车气动外形设计
2.
Aerodynamics Design and Store Separation Research of an Aviation Bomb;
某型号制导航弹气动外形设计及机弹分离气动特性研究
3.
Aerodynamic Configuration Design and Trajectory Simulation of an Interceptor Controlled by Aerodynamic/Lateral Thrust
气动力/直接力复合控制拦截弹的气动外形设计及弹道仿真
4.
An Effective Aerodynamic and Aeroelastic Coupled Design Method for Complicated Wing Shape
考虑气动弹性影响的机翼复杂气动外形设计研究
5.
Study on Smart Morphing Missile Aerodynamic Configuration Conceptual Design;
智能可变外形导弹的气动外形总体设计研究
6.
Genetic Algorithms and Their Applications to Aerodynamic Optimization Problems;
基因遗传算法及气动外形最优化设计
7.
Design of Configuration and Research of Aerodynamic Performance for Waverider Vehicles;
乘波飞行器外形设计与气动特性研究
8.
Design of shape and aerodynamic computing for low altitude & low speed manned airship
低空低速载人飞艇艇身外形设计及气动计算
9.
Integrated Design Method of Cruise Missile Including Configuration, Aerodynamics and Radar Stealth
巡航导弹外形/气动/雷达隐身综合设计方法
10.
Aerodynamic Characteristics Analysis and Design of Horizontal Axis Wind Turbine Blades
水平轴风力机叶片气动特性分析及外形设计
11.
Aerodynamic Shape Optimum Design Method for Guided Projectiles Equipped with Canards
鸭式制导炮弹气动外形优化设计方法研究
12.
Influence of Aerodynamic Shape Parameters on the Dynamic Characteristics of Missiles Based on Integrated Design
基于一体化设计的气动外形参数对动态特性的影响
13.
Research on Optimum Aerodynamic Design Using Simulated Annealing Algorithm and POD;
模拟退火结合正交分解算法的气动外形最优化设计
14.
Robust Optimization for Aerodynamic Design and Its Application to Design of a Micro Air Vehicle;
气动外形稳健优化方法及在微型飞行器设计中的应用
15.
Aerodynamic Design Based on Euler Equations and Discrete Adjoint Approach
基于Euler方程和离散共轭方法的气动外形优化设计
16.
Design and Experimental Verification of Hypersonic Inlet with Rectangular Section
矩形截面高超声速进气道气动设计及实验验证
17.
THEORETICAL DESIGN AND EXPERIMENTAL RESEARCH ON THE PNEUMATIC SHAPE MEASURING ROLL;
气动板形检测辊的理论设计及实验研究
18.
Design of Guidance Law for Exoatmospheric Interceptor During Its Terminal Course
大气层外动能拦截器末段导引规律设计