At different attack angles, Mach Numbers and ramp angles, the numerical calculations of inner and external flow field are performed for an adjustable mixedcompressioninlet.
对某可调混压进气道在不同攻角、不同马赫数、不同斜板角度下进行了大量的数值计算。
2
The uniform design and response surface methodology(RSM) are applied to the multi-objective optimization of a 2-D mixedcompression scramjet inlet.
基于响应面法进行了二维混合压缩超燃冲压发动机进气道的多目标优化研究。
3
The turbulent flow in 2 D mixedcompression supersonic inlet is simulated by numerical method.