Integrated design method of hypersonic slender body vehicle and three-dimensional inward turning inlet
A technology of hypersonic speed and design method, which is applied in the directions of aircraft parts, ground equipment, transportation and packaging, etc., to achieve the effect of high lift resistance characteristics and broaden the range of working Mach number
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[0026] like Figure 1~5 As shown, the integration scheme of the hypersonic slender body aircraft and the three-dimensional inward turning inlet includes the slender waverider aircraft precursor 23 and the three-dimensional inturning inlet, wherein the aspect ratio of the integrated device is 26, and the three-dimensional inner turning inlet The air inlet consists of a three-dimensional inner turning inlet compression surface 25, a three-dimensional inner turning inlet lip 26, a three-dimensional inner turning inlet shoulder 24, a three-dimensional inner turning inlet isolation section 21 and a three-dimensional inner turning inlet Transverse overflow port 28 is formed. And the three-dimensional inward turning inlet can realize internal wave riding. The front body 23 of the slender waverider aircraft and the three-dimensional inward turning inlet are connected and transitioned by means of the binary wedge guide band 20, and the three-dimensional inner turning inlet profile 25 ...
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