nose angle
英 [nəʊz ˈæŋɡl]
美 [noʊz ˈæŋɡl]
刀尖角
双语例句
- He looked up to discover that he had bent down the hollow nose needle at a twenty-degree angle.
他抬头一看，发现自己让中空的飞机机头向下倾斜了20度。 - In circumstances which cannot be ignored or avoided, daily occurrences right under people's nose are likely to be borrowed, from the angle of sociology, for the use of creative work.
天天发生在眼前的故事，在不能漠视也不能回避的情形下，从社会学角度，挪来为创作所用是可能的。 - This paper gives the analysis of a digital compensation method. The experimental results indicate that there are strict requirements for quantization accuracies of ship speed, nose angle, elevation angle, radar operating frequency and PRF, in performing this compensation.
本文分析了用数字方法进行舰速补偿，并作了实验，结果表明：这种补偿对舰速、舷角、仰角、雷达工作频率、重复频率代码等的量化精度都提出了严格要求。 - Vortex system and pressure distribution of slender bodies with elliptical cross-section nose at high angle of attack
大迎角下椭圆截面头部细长体的涡系和压强分布 - Experimental investigation on the formation mechanism of the effect of spin nose to asymmetric vortexes on slender body at high angle of attack
头部旋转对细长体大迎角不对称涡系影响机理的实验研究 - The nose exhalation gastric tube indwelling method could wide the opening angle of nasal valve area and efficiently judge the opening to increase the success rate of the indwelling gastric tube.
呼气法能增大鼻瓣区开口角度并有效判断开口位置，提高置管成功率。 - The duration of edema and the parameters of the width of the angulus oculi medialis, the height of ocular fissure, the height of radix nasi, the length of nose and the frontonasal angle were compared post operation.
术后比较肿胀消除时间以及内眦间距，眼裂高度，鼻根高，鼻长度和额鼻角等美学参数。 - A Method for Clearance Face Grinding of Major Cutting Edge of a Ball nose End Milling Cutter With Equal Orthogonal Clearance Angle
球头立铣刀端刃等主后角刃磨法 - Firstly, stability of a hypersonic boundary layer on a blunt cone with small nose bluntness at zero angle of attack has been investigated and the transition location was predicted by the e-N method.
首先，研究了高超音速零攻角小球头锥边界层的稳定性特点，并用e-N法进行了转捩预测。 - In this paper, the problem of transition prediction for supersonic and hypersonic boundary layers on a sharp or blunt nose cone at zero angle of attack or small angle of attack has been studied.
本文研究零攻角和小攻角、超音速和高超音速、尖锥和小钝头锥边界层的转捩预测问题。