1) empennage angle
尾翼角
2) Tail fin deflection
尾翼偏角
3) angle of stabilizer setting; (horizontal) stabilizer incidence
水平尾翼安装角
4) longitudinal dihedral angle
机翼和尾翼安装角之差
5) fin
[英][fɪn] [美][fɪn]
尾翼
1.
Based on the results of previous study , through optimization of the superplastic forming process and further tests, the paper puts forward an optimized scheme of superplastic forming process for an armour-piercing fin.
该成形方案使穿甲弹尾翼成形的自动化程度显著提高 ,产品质量更加稳定 ,劳动强度进一步减轻 ,生产率呈多倍提高 ,电能消耗大大减少 ,满足了大批量工业生产的要
2.
There are several types of fins adopted in the modern submarine,including mainly the X-fin and the 十-fin.
现代潜艇尾翼的形式普遍采用十字形和X形两种基本形式,文中通过采用求解RANS方程的数值计算方法,结合RNG-kε、S-kω、SST-kω3种湍流模型,对带有30°、45°,60°3种X形尾翼以及十字形尾翼的潜艇阻力进行数值模拟,通过计算结果发现:对各种方案采用RNG-kε和SST-kω湍流模型进行计算时,阻力比较接近,而采用S-kω湍流模型时,阻力比前两种要大;在所有方案中,45°尾翼具有最小的阻力。
3.
An explosively formed penetrator (EFP) with fins has the advantages of stable flight and deep penetration.
带尾翼的杆状爆炸成形侵彻体 ( explosively formed penetrator,简称 EFP)具有良好的飞行稳定性和侵彻性能 。
6) empennage
[英]['empinidʒ] [美]['ɛmpɪnɪdʒ]
尾翼
1.
The effect of empennage spread on flight attitude was analyzed and validated by flight test data.
针对某型导弹尾翼展开过程对飞行姿态的影响进行了细致地分析,并通过飞行试验数据对分析方法加以验证;最后论证了尾翼展开的不同步性会影响导弹的飞行姿态。
2.
Analyze the impact of empennage on the pose control of FMAVs and develop the moment model.
研究了尾翼对微扑翼飞行器姿态控制的影响,提出了尾翼对机身的力矩模型。
3.
Existing producing condition of complex empennage (aluminum alloy LD10) faces many problems, such as poor precision, weak mechanical properties.
针对复杂尾翼件 ( LD1 0 )生产中存在的精度低、力学性能差的实际问题 ,研究了尾翼等温成型技术 ,并优化了工艺参数。
补充资料：垂直尾翼
见尾翼。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条