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 -> 二元机翼
1.
Supersonic Nonlinear Fluutre Analysis of Dualistic Airfoil;
超音速流中二元机翼非线性颤振研究
2.
A Study of the Simulation of the Active Flutter Suppression of the Two-dimensional Wing Section
二元机翼颤振主动抑制的模拟仿真研究
3.
Aerodynamic Flutter and Limited Cycle of a 2-D Wing in the Hypersonic/Supersonic Flow Field
超声速/高超声速流中二元机翼的颤振与极限环
4.
Aerodynamic flutter and limited cycle of a 2-D wing in the supersonic flow field
超音速流中二元机翼的气动颤振与极限环
5.
Pulsation response of a two dimensional wing to atmosphere turbulence in supersonic flow
大气紊流作用下超音速二元机翼的脉动响应
6.
First Passage of a Two-Dimensional Airfoil Model Subject to Stochastic Parametric Excitation
二元机翼模型在随机参数激励下的首次穿越问题
7.
Random bifurcation and power spectrum analysis of a 2-dof airfoil with freeplay nonlinearity in pitch
具有间隙非线性的二元机翼的随机分岔和功率谱分析
8.
Numerical Analysis on a Two-degree-of-freedom Self-excited Airfoil with Asymmetry Freeplay Model;
具有不对称间隙的二元机翼自激振动的数值分析
9.
The Aeroelastic Flutter and Its Active Control of a 2-D Airfoil with a Control Surface
带操纵面二元机翼的气动弹性颤振及其主动抑制
10.
Effect of Control Surface Freeplay on Nonlinear Aeroelastic Responses of an Airfoil
控制面间隙对非线性二元机翼气动弹性响应的影响
11.
A chaos analysis of a two-dimensional airfoil with asymmetry freeplay
具有不对称间隙的二元机翼自激振动的混沌分析
12.
Secondary Development on Load Module of Airfoil FEM in MSC.PATRAN
在MSC.PATRAN中机翼有限元模型加载模块的二次开发
13.
Finite Element Analysis on Wings of Flapping-Wing Micro Air Vehicles Based on Dragonfly Wings;
基于蜻蜓翅翼的仿生微扑翼飞行器机翼的有限元分析
14.
Nonlinear Finite Element Analysis of Wing-Fuselage Connection Joint
机翼机身对接接头非线性有限元分析
15.
A Modeling Research of the Wing Finite Element Analysis with ANSYS;
ANSYS用于机翼有限元分析的建模研究
16.
Finite Element Analysis of a Composite Wing Based on MSC.NASTRAN
基于MSC.NASTRAN的复合材料机翼有限元分析
17.
The idea to create an aeroplane based on a blended wing and body, one that looks like a flying wing, is an old one.
这种将机翼和机身合二为一,使整个机身看似飞翼的设计由来已久。
18.
A Study of Low-Reynolds-Number Performance Over a Two-Dimensional Airfoil for Micro-Air Vehilce;
微型飞行器低雷诺数二元翼型的气动特性研究