1.
NUMERICAL STUDY ON THE SLENDER BODY AT HIGH ANGLE OF ATTACK
细长旋成体大迎角分离控制数值研究
2.
The development of high angle of attack test equipment in the 8m×6m low speed wind tunnel
8m×6m风洞特大迎角试验设备研制
3.
Numerical Investigation of Unsteady Aerodynamic Characterisics of Pitching Delta Wings
三角翼大迎角俯仰运动气动特性数值研究
4.
Frequency characteristics of breakdown vortices over delta wings with small amplitude oscillation at the high angle of attack
大迎角下小振幅振荡三角翼破裂涡的频率特性
5.
Experimental investigation on pressure distribution characteristics of wings of ×× missile at supersonic speeds and high angles of attack
××导弹翼面超声速大迎角压力分布特性试验研究
6.
Nonlinear Dynamic Characteristics Analysis and Control of Aircraft at High-Angle-of-Attack;
飞机大迎角非线性动力学特性分析与控制
7.
Computation of Vehicle Pitching Static and Dynamic Derivatives at High Angles of Attack
飞行器大迎角下俯仰静、动导数的数值计算
8.
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
9.
Research of Aerodynamic Characteristics for Double-bend Inlet in the Situation of High Incidence and Low Speed
低速大迎角下机腹双弯涵道空气动力性质研究
10.
DELAYED RANS/LES Method For High Attack Angle Flow over Multi-element Airfoil
多段翼型大迎角分离流动的DELAYED RANS/LES混合算法
11.
Research on the Aeroelastic Characteristics of an Airfoil in Moderate and High Incidences
中等及大迎角下的翼型气动弹性性质研究
12.
Capturing Details of Secondary Separation and Successfully Simulating Strongly Unsteady Turbulence Flow in Vortex Breakdown Region
基于层流假设的三角翼大迎角绕流特性数值模拟研究
13.
On an Unsteady Aerodynamics Model for Pitching-Oscillating Body at High Angle of Attack
飞行器快速俯仰产生大迎角非定常气动力数学模型研究
14.
Research on Flight and Control of the TV Fighter s Post-Stall Maneuvers;
推力矢量飞机过失速机动仿真研究及大迎角非线性控制律设计
15.
Lateral-Direction Aerodynamic Characteristics and Forebody Strake Control of an Aircraft Undergoing Pitching Oscillation on High Attack Angle
飞机大迎角俯仰运动下的横侧向气动特性及被动控制
16.
An Ecological Analysis of Death Comes for the Archbishop;
《死神来迎接大主教》的生态视角解读
17.
so does the ratio of lift anddrag, it gains only with the increase of the angle of release and goes to the maximum when the release angle is 25°.
升阻比和出手初速关系不大,它随迎角的加大而增大,迎角25°时达最大值。
18.
Effects of Vortex Generators on Maximum Lift and Stall Angle of Attack over Wings
旋涡发生器对机翼最大升力和失速迎角的影响