| 高超声速三维内收缩式进气道/乘波前体一体化设计研究评述 |
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| 引用本文： | 尤延铖,梁德旺,郭荣伟,黄国平.高超声速三维内收缩式进气道/乘波前体一体化设计研究评述[J].力学进展,2009,39(5):513-525. |
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| 作者姓名： | 尤延铖 梁德旺 郭荣伟 黄国平 |
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| 作者单位： | 南京航空航天大学能源与动力学院 |
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| 摘 要： | 论述了国内外在高超声速三维内收缩式进气道研究方面的最新研究动态,
重点阐述了三维变截面内乘波式进气道的研究进展.
介绍了常规矩形进口进气道与乘波体外形一体化相关研究,
并对三维内收缩式进气道与前体的一体化问题提出了关注. 最后,
对高超声速进气道与前体一体化设计的研究趋势进行了展望,
提出三维内收缩式进气道与乘波前体的``双乘波'一体化设计可能为高超声速研究带来新的变革.
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| 关 键 词： | 高超声速进气道 内收缩式 内乘波 乘波前体 双乘波 一体化 |
| 收稿时间： | 2008-07-03 |
| 修稿时间： | 2008-10-14 |
OVERVIEW OF THE INTEGRATION OF THREE-DIMENSIONAL INWARD TURNING HYPERSONIC INLET AND WAVERIDER FOREBODY |
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| YOU Yancheng
,
LIANG Dewang
,
GUO Rongwei
,
HUANG Guoping.OVERVIEW OF THE INTEGRATION OF THREE-DIMENSIONAL INWARD TURNING HYPERSONIC INLET AND WAVERIDER FOREBODY[J].Advances in Mechanics,2009,39(5):513-525. |
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| Authors: | YOU Yancheng LIANG Dewang GUO Rongwei HUANG Guoping |
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| Abstract: | The development of
airbreathing hypersonic vehicles is one of the focuses in
international competition for near space flight. The latest
research of three-dimensional inward turning hypersonic inlet is
presented, and some recent research results of the
section-controllable internal waverider hypersonic inlet in IFRC
of NUAA, China is proposed in detail. On the integration of
hypersonic inlet and waverider forebody, typical jobs between
rectangular two-dimensional and waverider airframe are reported
and the integration of three-dimensional inward turning hypersonic
inlet and waverider forebody is also elaborated. The future
development trend is suggested for both the hypersonic inlet and
airframe-propulsion integration, and a new concept of
dual-waverider is finally proposed. |
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| Keywords: | Hypersonic Inlet Inward Turning Internal Waverider Waverider Forebody Dual Waverider Airframe-Propulsion Integration |
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