青年中文supersonic inlet的意思
supersonic inlet中文翻譯：
超聲速進氣道
inlet───v.引進;嵌入;插入;；n.入口，進口；插入物；水灣
inlet elbow───進口彎頭
inlet grove───入口槽
water inlet───進水口; 進水管；[建]進水口，吸水口
inlet definition───入口定義
inlet wildwood───入口原木
inlet valve───進氣閥; 進給閥; 吸油閥; 吸入閥；[機]進氣閥；[機]進給閥
bogue inlet───[地名] [美國] 博格灣
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.───超聲速進氣道的性能優劣決定了補燃室流場內的壓強和空氣流量，進而影響到沖壓發動機的工作性能。
The turbulent flow in 2 D mixed compression supersonic inlet is simulated by numerical method.───對二元混壓超音速進氣道湍流流場進行了數值模擬。
The numerical simulation of supersonic inlet internal turbulent flow of solid rocket ramjet assisted range projectiles was performed by 2-order implicit TVD.───隱式TVD格式對固體火箭沖壓發動機增程彈丸超音速進氣道內部湍流流場進行了數值仿真。
The J-10B features a chin-mounted diffuser supersonic inlet (DSI) air inlet.───J-10B的顯著特征是機頭下方的無附面層隔道超音速進氣道（DSI）。
Numerical Study of the Dynamics Performance of a Supersonic Inlet for Air-Breathing Pulse Detonation Engine───自吸氣脈沖爆震發動機超聲速進氣道氣動性能的數值研究
Numerical Simulation and Experimental Validation of Flow in Mixed-Compression Axisymmetric Supersonic Inlet with Fixed-Geometry───定幾何混壓式軸對稱超聲速進氣道氣動特性數值仿真和實驗驗證
Numerical simulation of compressible and incompressible flows in mix-compression axisymmetric supersonic inlet───超聲速進氣道可壓及不可壓流動數值模擬
Numerical Simulation of a Mixed-Compression Supersonic Inlet Flow───混壓式超聲速進氣道流場數值模擬
The Numerical Investigation of Influence of Compression Face Position for Supersonic Inlet Performance───壓縮面位置對超聲速進氣道性能影響的數值研究
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.