1.
RCS of creeping wave for shadow region of wing leading edge
三维机翼前缘影区爬行波RCS研究
2.
NONLINEAR SUPERSONIC POTENTIAL FLOW OVER SIDESLIP CONICAL BODIES DELTA WINGS AND FUSELAGES
绕侧滑锥体、三维机翼与机身的超音速非线性全位势流计算
3.
Faster but Still Accurate Calculation of Wing Flutter Using Unsteady Transonic Euler Equations with Approximate Boundary Conditions
基于近似边界条件的三维机翼气动弹性数值模拟研究
4.
On this base, the static aeroelastics problems of wing and aircraft are investigated by coupled with structure dynamic equation.
并在此基础上耦合结构力学方程研究了三维机翼以及全机的静气动弹性问题。
5.
This paper presents a ALGOL program for calculating the thickness pressure distributions of arbitrary supersonic three dimensional wings by using the method of source singularities.
本文提供了用超音速源汇法计算任意三维机翼超音速厚度压强分布的算法语言程序。
6.
Aerofoil Sub-wainscot Wing-rib Join-hole Structure Fracture Characteristics Research Based on 3D Contact Problem
含三维接触问题的机翼下壁板翼肋对接孔结构断裂特性研究
7.
Aerodynamic Computation of 3-D Unsteady Euler Equations for Wings with Control Surface;
三维带操纵面机翼Euler方程非定常气动力计算
8.
Numerical simulation of SRM with finocyl grain during ignition transient
翼柱形药柱发动机点火瞬态三维数值模拟
9.
An airplane with wings placed above each other in three levels.
三翼机具有三个重叠的机翼的飞机
10.
Numerical Research on Three-dimensional Unsteady Flow Field of Micro Air Vehicle and Aerodynamic Optimization;
微型飞行器机翼三维非定常流场的数值研究和气动优化
11.
slim-delta aircraft
小展弦比三角翼飞机
12.
Computational Analysis on the Aerodynamic Characteristics of Combined Wing of WIG Craft
地效翼艇三维组合翼气动特性计算分析
13.
Maneuver Load Optimal Distribution Between Canard and Horizontal Tail of Three-surface Aircraft
三翼面飞机前翼和平尾机动载荷优化配置
14.
Numerical Simulation Study of Performance of Empennage Forming of Liner with Five Concave Arc Margins Cutted
五凹弧切边罩尾翼成形三维模拟研究
15.
delta wing (hang gliders)
三角形机翼（悬挂式滑翔机）
16.
Numerical Simulation of Unsteady Flows Past a Delta Wing by a 3-D Vortex Method;
三角翼周围非定常流动的三维涡方法数值模拟
17.
3D simulation of over-turned explosively formed projectile(EFP) with star-shaped fins
带尾翼的翻转型爆炸成形弹丸的三维数值模拟
18.
Transition studies for the boundary layer on a swept wing based on sublimation technique
基于升华法实验研究后掠翼三维边界层的转捩