high attack angle的例句大全

Analysis of Departure/ Spin Characteristics of F-16 at High Angle of Attack

F-16飞机大迎角飞行偏离/尾旋特性分析

The influence of nonlinear term to normal force coefficient and pitching moment coefficient caused by the detached air flow phenomenon in high angle of attack is mainly studied. The computing program related to this research is developed.

主要研究在大攻角下，气流分离现象所产生的非线性项对法向力系数和俯仰力矩系数的相互影响及其计算程序。

Investigation of improving the lateral static stability for the aircraft applied to high-subsonic flow and high angle of attack

某型飞机高亚声速大迎角横向静稳定性改善研究

The flow over delta wing with 65 ° and 70 ° swept at high angle of attack is investigated by solving the three dimensional, compressible Navier Stokes equations utilizing the second order upwind TVD algorithm ( Harten Yee).

采用Harten－Yee的二阶精度隐式TVD格式对N－S方程进行数值模拟，研究了后掠角为65°和70°的三角翼绕流的流场特性。

A wall correction at high angle of attack in low-speed wind tunnel using wall pressure signature method

壁压信息法低速大攻角洞壁干扰修正

A High Angle of Attack Dynamical System Identification Algorithm Based on LS-SVM

基于LS-SVM飞机大迎角动态辨识方法研究

it takes the interference velocity undulation into account for the aerodynamic forces and pitching moment corrections to solve the difficult moment correction problem in high angle of attack tests.

修正中考虑了洞壁干扰修正量分布不均匀的影响，初步解决了大迎角实验洞壁干扰修正中最困难的力矩修正问题。

High angle of attack wind tunnel test techniques is necessary for development of high-maneuverability flight vehicles.

大迎角风洞试验技术是先进高机动飞行器研制必需的关键技术.

The angle of attack of the high-aspect-ratio wings varies largely as the airflow rounds the airfoil.

在飞行状态下气流绕过翼型时,大展弦比机翼的迎角变化范围非常大.

The Advance of Aircraft Flying Qualities Researching at High Angle of Attack

飞机大迎角飞行品质研究的进展

Application of the wall pressure method to wall interference corrections for model tests at high angle of attack in high speed wind tunnel

壁压法应用于高速风洞大迎角实验洞壁干扰的修正

Dynamic aerodynamics characteristic is one of very important parameters of modern maneuverable aircraft to be scaled at high angle of attack and high speed.

高速大迎角动态气动特性是衡量新一代高机动飞行器性能的重要参数之一。

The results of flight test show that JL8 aircraft has very good characteristics of high angle of attack, low speed and high speed stalls.

试飞结果表明，JL8飞机具有良好的大迎角特性及低速和高速失速特性。