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单词 angles of attack
释义

angles of attack

例句

释义:
1.
Aeroelastic analysis at high angles of attack is an attractive and complicated research subject in modern aircraft design.
大迎角气动弹性分析是现代飞行器设计中非常引人瞩目并且复杂的研究课题。
hkxb.buaa.edu.cn
2.
With one possible eleventh-hour exception, attempts to find alternative angles of attack have not shown conspicuous success.
但11月还没到,共和党的如意算盘就出现意外,这时再另找攻击点可能不会奏效。
www.bing.com
3.
The investigated range of speeds and angles of attack greater than the values encountered in normal operation of the aircraft.
研究的飞行速度范围和攻角比日常飞行中遇到的要大。
www.5i8866.com
4.
The required lateral maneuver trajectory on equilibrium glide assumption is specified according to the designed angles of attack and bank.
根据所设计的攻角和倾侧角,即可实现平衡滑翔情况下预定机动模式的侧向机动。
hkxb.buaa.edu.cn
5.
We just have different angles of attack on this general problem.
只是对这一普遍的问题有不同的着手点。
open.163.com
6.
The airplane rolls and performs great at extremely high angles of attack.
这架飞机可以在极大迎角状态下横滚并表现优异。
www.fyjs.cn
7.
The experimental model and equipment are designed, and the low speed wind tunnel experiment at high angles of attack is made.
设计了模型和实验装置,进行了大迎角低速风洞实验。
sylx.ustc.edu.cn
8.
Jigs for ailerons and tail angles of attack.
用以保证副翼及尾翼安装角的夹具。
www.turbomoni.com
9.
The research of effect of flow turbulence on the aerodynamic characteristics of a wing-body combination at high angles of attack
湍流度对翼身组合体大攻角气动特性的影响研究
ilib.cn
10.
Primal research of the effect of flow turbulence on aerodynamic characteristics of a aircraft model at high angles of attack
湍流度对飞行器模型大迎角气动特性影响的初步研究
ilib.cn
1.
Experimental Study on the Flow Patterns of a Simplified Aircraft Model at High Angles of Attack
某型号飞机简化模型大攻角流态初步研究
www.ilib.cn
2.
Vortices structure and pressure fluctuation characteristics of the flow over slender body at high angles of attack
细长旋成体大迎角绕流的背涡结构与压力脉动特性
ilib.cn
3.
Numerical Investigation of Asymmetric Vortical Flow over a Slender Body at Large Angles of Attack
细长体大攻角非对称涡流的数值研究
ilib.cn
4.
Experimental study of non-stationarity in the flow over slender body at high angles of attack
细长旋成体大迎角绕流非定常特性的实验研究
ilib.cn
5.
The unsteadiness study of nose vortices in the flow over slender body at high angles of attack
大迎角细长体头涡结构演变的非定常现象研究
ilib.cn
6.
Correlative Analysis between Pressure Distributions and Vortex Pattern of Double-Delta Wings at High Angles of Attack
双三角翼大迎角翼面压强分布与涡态相关分析
www.ilib.cn
7.
Effects of grit strip on flow asymmetry over a slender revolution body at high angles of attack
粗糙带对细长体大迎角流动非对称性的影响
ilib.cn
8.
Calculation of pressure distributions of low aspect ratio missile wings at supersonic speeds and high angles of attack
超声速大迎角条件下小展弦比弹翼压力分布计算研究
ilib.cn
9.
Numerical simulation of swimming of two hand-figures at various angles of attack
两种手姿态在不同攻角下划水的数值模拟
www.ilib.cn
10.
Analysis on Sensitivity of High Angles of Attack Longitudinal Flying Qualities to Variation of Parameters
纵向大迎角飞行品质对参数的灵敏度分析
www.ilib.cn
1.
Computation of Field Structure and Aerodynamic Characteristics of Delta Wings at High Angles of Attack
三角翼大迎角流场结构和气动力特性的计算分析研究
scholar.ilib.cn
2.
High Angles of Attack Character Analysis and Test for an Advanced Fighter
先进战斗机大迎角运动特性分析和试验
ilib.cn
3.
The characteristics of nose vortices and Karman vortices in the flow over slender body at high angles of attack
细长旋成体大迎角绕流中的头涡与卡门涡的脉动压力特性
ilib.cn
4.
Numerical Inversigation of Field Structure and Aerodynamic Characteristics of Delta Wings at High Angles of Attack
三角翼大迎角流场结构和气动力特性的数值分析研究
www.ilib.cn
5.
Effect of Dorsal Fin Height on Symmetry and Asymmetry of Vortex Pairs over Delta Wing at High Angles of Attack
背鳍对三角翼大迎角脱体涡的影响
ilib.cn
6.
Application of Bifurcation Analysis to Control Law Design at High Angles of Attack
分叉分析方法在大迎角控制律设计中的应用
ilib.cn
7.
Development of the balance for crew escape system at large angles of attack and sideslip angles
弹射救生系统大迎角大侧滑角天平设计研究
www.ilib.cn
8.
Calculation of roll torque in effect of ablation lag for spinning blunted cone at angles of attack
有迎角旋转钝锥的烧蚀滞后滚转力矩的算法
www.ilib.cn
9.
Parallel Computations of Flow Around A Double-Delta Wing at High Angles of Attack
双三角翼大迎角绕流的并行计算
168.160.184.82:8080
10.
Stable Field Analysis of Aircraft Flying at High Angles of Attack
飞机大攻角俯仰飞行的稳定域分析
www.ilib.cn
1.
Asymmetric vortex structure of slender revolution at high angles of attack
细长尖头旋成体大迎角非对称涡系结构
ilib.cn
2.
The study on the test uncertainty level at high angles of attack for domestic capital low-speed wind tunnels
国内主力低速风洞大迎角实验的不确定度水平研究
ilib.cn
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更新时间:2024/11/9 4:00:41