三角翼飞机

机身边条对双三角翼飞机升力特性的影响

The effects of body-strake on lift characteristics of the double-delta-wing aircraft

双三角翼飞机气动力工程计算研究

Engineering Calculation Research of Aerodynamics for Aircraft with Double Delta Wing Configuration

通过低速风洞测力试验和七孔探针对空间流场的测量，研究了机身边条对双三角翼飞机升力特性的影响，并分析了机身边条的增升机理。

This article introduced the study of seven hole hollow fiber with spiral three dimensional crimps and the technologic improvement on producing stabilization and higher product quality .

采用基于面积比思想的半经验工程算法计算了双三角翼飞机的升力系数曲线斜率、零升阻力系数和诱导阻力因子。

By using the semi experiential engineering arithmetic based on the ideology of area ratio , the slope of lift coefficient curve , the zero lift drag coefficient and the induced drag factor of double delta wing aircraft were calculated .

在过去的70年，他们已经为包括三角翼，无尾飞机发展的试验场，和超音速飞行。

Over the last seven decades , they 've been a proving ground for developments including delta wings , tailless aircraft , and supersonic flight .