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angle of attack相关的网络例句

查询词典 angle of attack

与 angle of attack 相关的网络例句 [注:此内容来源于网络,仅供参考]

Just similar to changing the attack angle of aerofoil.

其作用与改变翼型的迎角类似。

In the example illustrated here, flight conditions are: altitude of 700 m, speed of 55 m/s, and attack angle of 0 degrees.

在这里的例子说明,飞行条件是:海拔700米,速度55米/秒,和攻角在0度。

The results show that the inclined walls and the change of attack angle have great influence on the pressure distributing and St.

结果表明,倾斜壁面和攻角改变对压力分布和St有较大影响。

Aiming at improvement of attack precision and reduction of target miss distance, different guidance and control laws are proposed and analyzed, the influences of many different kind of conditions to attack precision such as initial flying altitude, airspeed, flight path angle, external disturbance and target movement are investigated. Beneficial to theoretical significance and inspiring for engineering practice results are obtained.

紧紧围绕提高末制导精度、减小脱靶量这一研究目的,对不同的末制导控制方式、不同的末制导导引律、不同的末制导进入条件、不同的外部干扰、不同的目标特性等都进行了深入的研究、分析和探讨,并给出具有一定理论意义和丰富的工程实际应用价值的结论。

In addition, the computational evaluations indicate that the heat transfer enhancement of delta winglet for aligned tube bank heat exchanger is more significant than that for staggered tube bank heat exchanger, the heat transfer enhancement of delta winglet with the attack angle of 45° is more obvious than that of 30°; the delta winglet with the attack angle of 45° leads to an increase in pressure drop, while the delta winglet with the attack angle of 30° results in a slight decrease.

另外计算还发现:三角形小翼对顺排换热器的强化换热效果好于对叉排换热器的强化;冲角为45°的三角形小翼强化换热效果好于冲角为30°的三角形小翼;冲角为45°的三角形小翼导致空气压降提高,而冲角为30°的三角形小翼则可使压降有所减小。

From the angle of manmade unauthorized passive wiretapping and attack network this paper analyzes the main problems and solution about network information safe and gives a simple description about function and application of antifire wall.

文章从人为故意的未授权窃取、攻击网络的角度,分析了网络信息安全的主要问题及对策,并就防火墙的功能及应用作了简要说明

In this paper, The delta wing of Mach number 0.8 at an attack angle of 21. 8 degree is simulated by our program. Then, using the visualizing program, we map the figures of space streamlines, cross streamlines near the vortex axis, three dimensional vortex lines, cloud atlas for pressure and vortex and targer of particles.

在这一章里,我们先用所建立的计算软件数值模拟了来流马赫数为0.8、攻角为21.8°的三角翼的流场,之后以拓扑分析结果做指导,研制了一套数值显示流场、旋涡结构的软件,用该软件我们绘制了跨音速三角翼背风区涡轴附近截面流线、空间流线、三维涡量线、压力和涡量云图以及粒子屏痕图。

Viscous flows around an infinite span untapered swept back wing at high angles of attack are investigated numerically by solving the quasi two dimensional Navier Stokes equations to deal with the effects of the swept-angle on the flow structure and force behavior.

通过数值求解Navier Stokes方程,研究了无限翼展直后掠翼在不同后掠角下的大迎角粘性分离流,探讨了后掠角对流场结构和升阻力特性的影响。

Results show that the incre asing of attack angle,the total pressure recovery chanˉ ges a little and mass flow ratio reduces.However,flow distortionind ex increasers obviously.

结果显示,随着来流攻角的增大,此进气道总压恢复系数变化不大,流量系数逐渐降低,而流场畸变则明显增大。

The simulation study mainly concentrates on the following aspects: the relations of attack angle versus caudal fin motion, the phase difference of heaving and pitching motion of caudal fin motion, swimming velocity and body motion, body wave length and body motion, heaving amplitude and body motion, Strouhal Number and body motion.

具体研究内容包括:最大击水角度对尾鳍运动的影响;尾鳍摆动—平动运动相位差对尾鳍运动的影响;游动速度对鱼体运动的影响;鱼体波波长对鱼体运动的影响;尾鳍后缘最大摆幅对鱼体运动的影响;斯德鲁哈尔数对鱼体运动的影响。

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