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单词 supersonic inlet
释义

supersonic inlet

美 
英 
  • un.超音速进气道
  • 网络超声速进气道
un.
1.
超音速进气道

例句

释义:
1.
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)。
www.bing.com
2.
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
www.ilib.cn
3.
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
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4.
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
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5.
Numerical Simulation of a Mixed-Compression Supersonic Inlet Flow
混压式超声速进气道流场数值模拟
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6.
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
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7.
Stern Shape Design and Numerical Study of Base Drag for Supersonic Inlet Fairing
超声速进气道整流罩船尾形状及其底阻的数值研究
www.ilib.cn
8.
Numerical Solution of Three Dimensional Supersonic Inlet Systems by Domain Decomposition Method
三维超音进气道系统流场计算的区域分裂算法
168.160.184.78
9.
Experiment on Stability for Mixed-Compression Axisymmetric Supersonic Inlet with Fixed-Geometry
定几何混压式轴对称超声速进气道的稳定性实验
scholar.ilib.cn
10.
Real time mathematical model of supersonic inlet of a turbofan engine
涡扇发动机超声速进气道实时数学模型
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1.
Static Internal Performance Analysis and Numerical Simulation of Supersonic Inlet
超声速进气道内特性数值模拟及性能分析
www.ilib.cn
2.
Calculation of Additive Drag of Supersonic Inlet under Subcritical Operating Condition
超声速进气道在亚临界条件下的附加阻力的计算
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3.
Investigation of Supersonic Inlet Mathematical Model with Attack Angle
超音速进气道建模方法研究
www.ilib.cn
4.
Modeling supersonic inlet boundary layer bleed roughness
超音速进气道边界层吸除粗糙度的模拟
lib.buaa.edu.cn
5.
Study for the mathematical model of supersonic inlet
超声速进气道数学模型研究
www.ilib.cn
6.
Analysis of Suction Roles for Supersonic Inlet on Combined Engine
某组合发动机进气道抽吸作用分析
www.ilib.cn
7.
Integrative design of supersonic inlet and missile body
超声速进气道与弹体一体化外形研究
www.ilib.cn
8.
Experiment study on supersonic inlet in dual-model scramjet
双模态冲压发动机高超进气道的实验研究
www.ilib.cn
9.
Matching between supersonic inlet and aero-engine
超声速进气道与发动机的匹配
www.ilib.cn
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更新时间:2025/1/27 10:23:06