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1)  delta winged body
三角翼体模型
2)  submerged triangle wing
潜没式三角翼体
1.
Analyze of the properties of the submerged triangle wing for adjusting shallow supercritical flow;
控导浅层急流的潜没式三角翼体特性研究
3)  triangle model
三角模型
1.
The triangle model can serve as an intuitive platform for illustrating existing sustainability status and trends in economic development coincident with the implementation of various measures.
根据区域经济发展、资源—能源消耗及环境污染的相互关系,结合生态学表现,基于三角模型工具及经济可持续发展定义,分析评估区域经济可持续发展状况和长期趋势。
2.
According to the necessity of distance measurement in four-legged league of RoboCup,this paper presents a method of distance measurement for Sony four-legged robot based on triangle model,which is more flexibility comparing with conventional distance measurement model based on color region.
针对RoboCup四腿机器人足球比赛中如何测定目标物体距离的问题,本文提出了一种基于三角模型的距离测定方法,与基于区域色块的距离测定算法相比,该方法不再依赖于图像色块信息,实现了在色块信息不可用情况下对目标物体距离的准确测定。
3.
The triangle model,as an intuitive platform for illustrating sustainability status and trends in economic development,seems to hold promise as an analytical management tool liable to be used by researchers and policy-makers at different levels due to its simplicity and flexibility.
三角模型作为一种直观的平台能够很好地图解区域可持续综合发展状况及长期趋势。
4)  delta wing
三角翼
1.
Numerical simulation of unsteady flows past a delta wing using a 3-D vortex method;
三角翼周围非定常流动的三维涡方法数值模拟
2.
Effects of free stream local disturbance on delta wing aerodynamics;
来流局部干扰对三角翼气动特性的影响
3.
Numerical simulation to effects of trailing edge jet on delta wing vortices;
后缘喷流对三角翼前缘涡影响的数值模拟
5)  double delta wing
双三角翼
1.
The effects of Gurney flap on double delta wing aerodynamic performance in low speed wind-tunnel tests;
Gurney襟翼对双三角翼气动特性影响的低速风洞实验研究
2.
Experimental investigation of the vortex characteristic over 75°/45°double delta wing;
75°/45°双三角翼旋涡特性的试验研究
3.
Compared with a delta wing aircraft, the double delta wing configuration has better aerodynamic performance at high angles of attack.
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。
6)  double-delta wing
双三角翼
1.
Experimental study on pressure measurement distribution of double-delta wings;
双三角翼压力测量实验研究
2.
The vortex visualization and surface pressure distribution for a 75°/45°double-delta wing were carried out in the water tunnel and in the low speed wind tunnel of BUAA.
本文通过风洞试验和水洞试验研究了75°/45°双三角翼的外翼前缘形状对大迎角分离流动的影响。
3.
The vortex visualization and surface pressure distribution measurement for a 75°/60° double-delta wing were carried out in the water tunnel and in the low speed wind tunnel of BUAA.
笔者对75°/60°双三角翼模型进行了水洞流态观测实验、低速风洞测压实验、空间流场测量实验,研究了双三角翼外翼前缘钝度对气动特性影响,包括对涡态的影响。
补充资料:三角翼飞机
三角翼飞机
delta-wing airplane

   机翼前缘后掠,后缘基本平直,半翼俯视平面形状为三角形的飞机。机翼重量轻、刚度好,有利于收置起落架,安放燃油和其他设备。三角翼超声速阻力小,从亚声速过渡到超声速时机翼压力中心向后移动量小,这对于舵面平衡能力比较差的飞机尤为重要,所以无尾飞机和鸭式飞机基本上都采用三角翼。超声速飞机也常用三角翼的形式,但由于超声速三角翼飞机展弦比较小,亚声速飞行时的升阻比低,故亚声速巡航特性不好。小展弦比的三角翼只有在大迎角下有足够升力系数,因飞机着陆前迎角不能很大,故其着陆性能较差。
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