2) S-shaped inlet
S弯进气道
1.
Experimental investigation of pneumatic characteristics for S-shaped inlet in missiles
弹用S弯进气道气动性能试验
2.
An investigation on the ventral diverterless high offset S-shaped inlet is carried out at Mach numbers from 0.
针对腹下无隔道大偏距跨声速S弯进气道开展了高速吹风实验研究,并对得到的图谱和曲线进行了分析。
3.
According to structural features of the active unmanned aerial vehicle(UAV) inlet,a bilateral type S-shaped inlet with large offset and short diffuser is designed.
根据现役无人机进气道的结构特点,以后置两侧布局的S弯进气道作为研究对象,完成了一种大偏距、短扩压S弯进气道设计,设计包括中心线、面积变化规律选取以及斜切唇口等;并且对设计模型进行风洞实验研究,得到进气道的速度特性、攻角特性和偏航角特性等。
3) S-shaped inlet
S形进气道
1.
Numerical simulation of flow field for supersonic S-shaped inlet;
S形进气道流场数值模拟
2.
The three dimensional turbulent flows inside/outside the supersonic S-shaped inlet were numerically studied for various flight conditions.
论文对超音速S形进气道内外流场进行了数值计算研究,分析了不同飞行条件下进气道的流场及出口流场品质,并探索利用增加扰流柱的方法减小进气道出口流场畸变,计算结果与实验数据符合良好。
4) S shaped inlet
S弯进气道
1.
Considering the structure characters (large offset and short diffuser) of missile inlet, a design method of the S shaped inlets for a high subsonic missiles is presented.
针对导弹进气道的结构特点 ,在前人的工作基础上总结出一种适合导弹使用的大偏距、短扩压 S弯进气道的设计方法。
5) short S-shaped intake duct
短S弯进气道
1.
Three-dimensional viscous flowfield numerical simulation for a short S-shaped intake duct is performed.
对短S弯进气道进行了三维粘性流场的数值模拟。
补充资料：[3-(aminosulfonyl)-4-chloro-N-(2.3-dihydro-2-methyl-1H-indol-1-yl)benzamide]
分子式：C16H16ClN3O3S
分子量：365.5
CAS号：26807-65-8
性质：暂无
制备方法：暂无
用途：用于轻、中度原发性高血压。
分子量：365.5
CAS号：26807-65-8
性质：暂无
制备方法：暂无
用途：用于轻、中度原发性高血压。
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