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1)  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。
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。
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3)  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。
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4)  S-shaped inlet design
S弯进气道设计
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5)  ventral S-shaped inlet
腹下S弯进气道
1.
Investigation of pneumatic characteristics for a ventral S-shaped inlet at high incidence and low speed;
一种腹下S弯进气道低速大攻角下气动特性实验
6)  short-S inlet duct
短S形进气道
1.
A numerical simulation of three-dimensionaol viscous flow for 5 different short-S inlet ducts has been performed using fluid analysis software FLUENT.
借助于流体分析软件对5种特定的短S形进气道进行了三维粘性流场的数值模拟。
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