应用隐式AF方法计算了为发动机进气道设计的典型扩压器内的复杂湍流流场。
A complicated turbulent flow field in a diffuser with typical geometric shape for aeroengine inlet design was calculated by the use of the implicit AF method.
以应用于实际设计为目的，研究了现代设计方法在发动机螺旋进气道设计中的应用。
In order to be used in practical design, application of modern design method for engine's helical intake ports is studied.
进行了多方案二元混压超声速进气道设计和筛选，确定了主设计方案，并完成试验研究。
Through many schemes design and filter of 2-D mixed-compression supersonic intake, confirm the design scheme of experimental investation.
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