A variant of the swept-back wing is the delta wing.
后掠翼的变型是三角翼。
It had a delta wing configuration with a single vertical tail.
它有一个三角翼和单向的垂直翼。
The same conclusion is obtained with different sweep delta wing configurations.
不同后掠角的三角翼均能得到相似的结论。
The Concorde's delta wing made the plane's sustained cruising speed of Mach 2 possible.
协和飞机的三角翼飞机作出的持续巡航速度2马赫的可能。
Micro balloon actuator array for aerodynamic control of delta wing has been explored in this paper.
本文就以用于三角翼气动控制的微气泡致动器阵列为对象展开研究。
The effects of Gurney flap on double delta wing aerodynamic performance in low speed wind-tunnel tests;
双三角翼气动布局比三角翼飞机具有更好的大攻角空气动力特性。
Numerical investigation of the effects of different leading-edge profiles on vortical flows over a double-delta wing;
计算模型包括尖前缘、菱形前缘、圆形前缘等三种不同前缘形状的机翼。
On the basis of the above, the mechanism is investigated by which the chine forebody can delay delta wing vortex burst.
在此基础上，对融合体前体延迟翼涡破裂的机理进行了深入探讨。
But the computer and an additional flight control device called the canard have rescued the delta wing from obsolescence.
但电脑和一额外的飞行控制装置，称为鸭已救出三角翼从陈旧。
Internal fuel fraction may also be high, given the fuselage configuration and large internal volume of the big delta wing.
内部油箱可能也很大，考虑到机身的尺寸和起巨大的三角翼的内部空间。
Optimization for the double delta wing platform of a new advanced trainer shows that the system is quite applicable and the results …
通过某机双三角机翼平面形状的优选，表明系统具有较高的实用性，并与工程实践相吻合。
Three-dimensional turbulent boundary layer on the ground board is measured through the ground effect tests of a delta wing with aspect ratio 3.
本文通过一个展弦比为3的三角形机翼的地面效应试验，测量了地板上的三元紊流附面层。
Velocity gradient, pressure gradient and circulation gradient are used to model the separated vortex flow field over a leading edge delta wing.
用速度梯度、压力梯度和环量梯度模拟大攻角尖前缘三角翼流场。
Optimization for the double delta wing platform of a new advanced trainer shows that the system is quite applicable and the results are in good...
通过某机双三角机翼平面形状的优选，表明系统具有较高的实用性，并与工程实践相吻合。
This paper provides valuable experimental results for the applied study of internal acoustic excitation of a two-dimensional airfoil or a delta wing.
本文将对二元翼型及三角翼等内部声激励的应用研究提供有价值的实验结果。
The micro shear stress sensor which based on the smart skin for boundary-layer separation point detection of delta wing has been explored in this paper.
本文就以用于实现三角翼边界层分离点检测的面向灵巧蒙皮的微型剪应力传感器为对象展开研究。
In this paper, the laser sheet technology is used to research the flow visualization of sections of double delta wing, and some important results are introduced.
介绍了采用激光片光技术在风洞中进行双三角翼剖面流动显示研究的方法和主要结果。
In order to study the wing rock characteristics of a fighter, the wing rock characteristics for a fighter with delta wing configuration is investigated in this paper.
为了研究战斗机的机翼摇滚特性，运用风洞试验和数值模拟手段，对一典型三角翼布局开展了研究工作。
The study shows that the LCO of a cropped delta wing is not only closely related to its geometric nonlinearity, but also remarkably affected by its material nonlinearity.
研究结果显示，切尖三角翼的L CO不仅与结构几何非线性密切相关，而且受到结构材料非线性的显著影响。
For lower inflow dynamic pressures, the LCO of the delta wing is caused by structural geometric nonlinearity, and the numerical results correlate well with experimental data.
在小来流动压情况下，结构几何非线性引起了切尖三角翼的LCO，计算结果和试验值吻合较好。
From the characteristics of aerothermoelasticity, the effects of temperature in aerodynamic heating on the mode of a delta wing and the characteristic of its flutter were researched.
根据热气动弹性特点，探讨了气动加热温度对三角机翼模态特性和颤振特性的影响。
Optimization for the double delta wing platform of a new advanced trainer shows that the system is quite applicable and the results are in good agreement with the engineering practice.
通过某机双三角机翼平面形状的优选，表明系统具有较高的实用性，并与工程实践相吻合。
The vortex flow field is calculated with difference methods, and the motion characteristics and the bursting mechanism of the leading-edge separated vortices of delta wing are analyzed.
采用差分方法计算旋涡流场，进而分析三角翼上前缘分离涡的运动特点及其破碎机理。
The results show that unsteady aerodynamic characteristics of a delta wing oscillating in large amplitude pitching roll motion are more complicated than in pitching motion or in roll motion.
结果表明，飞行器俯仰滚转耦合运动时的气动特性比单独俯仰和滚转时的气动特性复杂得多。
The calculated results indicate that the choice of the limiter function in TVD scheme has an important influence on the numerical simulation which is carried out on the delta wing flow structure.
计算结果表明：TVD格式中限制器函数的选取对于三角翼绕流结构的计算结果具有较重要的影响。
This paper deals with the numerical solution of the Euler equation for airfoils using approximate boundary conditions and the effects dorsal fin on vortex over delta wing at high angles of attack.
本论文主要是通过实验来研究细长圆锥体在大迎角下的绕流流场的特性和细长三角翼加背鳍后对前缘涡的影响，检验相关理论结果。
This paper deals with the numerical solution of the Euler equation for airfoils using approximate boundary conditions and the effects dorsal fin on vortex over delta wing at high angles of attack.
本论文主要是通过实验来研究细长圆锥体在大迎角下的绕流流场的特性和细长三角翼加背鳍后对前缘涡的影响，检验相关理论结果。
应用推荐