supersonic inlet信息详情
超声速进气道
inlet───v.引进;嵌入;插入;；n.入口，进口；插入物；水湾
inlet elbow───进口弯头
inlet grove───入口槽
water inlet───进水口; 进水管；[建]进水口，吸水口
inlet definition───入口定义
inlet wildwood───入口原木
inlet valve───进气阀; 进给阀; 吸油阀; 吸入阀；[机]进气阀；[机]进给阀
bogue inlet───[地名] [美国] 博格湾
inlet yoga───入口瑜伽
The performance of supersonic inlet determines the pressure and the air flux in combustor, then affect the work of ramjet.───超声速进气道的性能优劣决定了补燃室流场内的压强和空气流量，进而影响到冲压发动机的工作性能。
The turbulent flow in 2 D mixed compression supersonic inlet is simulated by numerical method.───对二元混压超音速进气道湍流流场进行了数值模拟。
The numerical simulation of supersonic inlet internal turbulent flow of solid rocket ramjet assisted range projectiles was performed by 2-order implicit TVD.───隐式TVD格式对固体火箭冲压发动机增程弹丸超音速进气道内部湍流流场进行了数值仿真。
The J-10B features a chin-mounted diffuser supersonic inlet (DSI) air inlet.───J-10B的显著特征是机头下方的无附面层隔道超音速进气道（DSI）。
Numerical Study of the Dynamics Performance of a Supersonic Inlet for Air-Breathing Pulse Detonation Engine───自吸气脉冲爆震发动机超声速进气道气动性能的数值研究
Numerical Simulation and Experimental Validation of Flow in Mixed-Compression Axisymmetric Supersonic Inlet with Fixed-Geometry───定几何混压式轴对称超声速进气道气动特性数值仿真和实验验证
Numerical simulation of compressible and incompressible flows in mix-compression axisymmetric supersonic inlet───超声速进气道可压及不可压流动数值模拟
Numerical Simulation of a Mixed-Compression Supersonic Inlet Flow───混压式超声速进气道流场数值模拟
The Numerical Investigation of Influence of Compression Face Position for Supersonic Inlet Performance───压缩面位置对超声速进气道性能影响的数值研究
Complex wave structures of supersonic inlet at critical status are achieved by numerical simulation, and analysis on flow structure characteristic and shock wave structure is made.
The investigation shows that the diverterless supersonic inlet or bump inlet creates a high pressure area on the bump compression surface which pushes the air in boundary layer away from the inlet.
By means of block structure grid and second-order zonal solver method, the research on supersonic inlet performance of solid rocket ramjet assisted range projectiles was carried out.
Complex wave structures of supersonic inlet at different angle of attack and spinning velocity related to high speed spinning and critical status were achieved.