two-dimensional inlet 二维进气道
three-dimensional inlet 三元进气道
three-dimensional sidewall inlet 三维侧压式进气道
two-dimensional supersonic inlet 二元超声速进气道
three-dimensional sidewall hypersonic inlet 三维侧压式高超声速进气道
By comparison of inlet total pressure recovery coefficient, attack-angle performance of chin inlet and two-dimensional inlet are superior to frontal inlet.
对不同布局的总压恢复系数进行比较，颌下及两侧进气则较头部进气有好的攻角特性。
In this paper, a FVM-TVD method for simulation of one-dimensional unsteady flow in inlet and exhaust manifold of ICE has been constructed.
介绍了进排气系统一维非定常流动的FVM- TVD法（总残差减少的有限体积法）。
The results show that the actual turbulent round jet flow must be simulated by a three-dimensional analysis with inlet perturbations.
分析了不加扰动和加扰动模拟的本质差异，指出准确预报实际圆湍射流流动应采用施加入口扰动的三维模拟。
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