There is a difference between the numerical simulation results of two-dimensional and three-dimensional flow field in supersonic inlet, which shows the influence of boundary layer on the side wall.
超声速进气道的三维流场数值模拟结果与二维数值模拟结果存在较明显的差别，说明进气道侧壁附面层的影响不容忽略；
The straight cell partition wall (22) has at an exhaust gas inlet-side end an introduction promoting unit (60) for promoting the introduction of exhaust gas into each straight cell (21).
直室隔壁（22）在排气入口侧端部具有促进排气向各直室（21）内导入的导入促进部（60）。
The straight cell partition wall (22) has at an exhaust gas inlet-side end an introduction promoting unit (60) for promoting the introduction of exhaust gas into each straight cell (21).
直室隔壁（22）在排气入口侧端部具有促进排气向各直室（21）内导入的导入促进部（60）。
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