Unique design method of subsonic inlet with complex cross-sectional shape

被引：0

作者：

Internal Flow Research Center, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China ^{[1
]}

不详 ^{[2
]}

机构：

来源：

Hangkong Dongli Xuebao | 2009年 / 6卷 / 1357-1363期

关键词：

Circular shape - Complex cross-sectional shaped inlet - Cross-sectional shape - Design method - Design procedure - Generating methods - Inlet design - Slot-shaped inlet;

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学科分类号：

摘要：

A cross-sectional shape generating method for subsonic inlet design was proposed according to curvature regulation. This unique method can realize the transition of an arbitrary entrance shape to the exit circular shape easily and smoothly. Utilizing this method, an inlet design procedure was programmed, which could accomplish the surface composition of subsonic inlet with complex cross-sectional shape and complex bending style quickly and graphically. As a preliminary application, several diffusers with different entrance shape were generated and especially the design procedure of a slot-shaped inlet like that of X-47 vehicle was described in detail.

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