| 浅析俄罗斯战斗机CY—37“金雕”前掠翼三翼面气动布局的先进性 |
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| 引用本文： | 陈正举.浅析俄罗斯战斗机CY—37“金雕”前掠翼三翼面气动布局的先进性[J].沈阳航空工业学院学报,1999,16(2):62-69. |
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| 作者姓名： | 陈正举 |
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| 作者单位： | 沈阳航空工业学院航空动力与热力工程系 |
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| 摘 要： | 本文追溯了前掠翼的飞机的渊源。指出常规二翼面的后掠翼，变后翼和近矩耦合鸭式气动布局存在着妨碍机动进一步提高的缺点。
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| 关 键 词： | 俄罗斯 战斗机 前掠翼 气动布局 |
Simple Analysis the Advantage of Russia's CY-37 "Jin Diao" Forward-Swept Wing and Triplanar Aircraft on Aero Configuration |
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| Chen Zhengju.Simple Analysis the Advantage of Russia''''s CY-37 "Jin Diao" Forward-Swept Wing and Triplanar Aircraft on Aero Configuration[J].Journal of Shenyang Institute of Aeronautical Engineering,1999,16(2):62-69. |
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| Authors: | Chen Zhengju |
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| Institution: | Chen Zhengju |
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| Abstract: | The origins of forwar - swept wing aireraft are described in this paper. Theexistent defects of normal biplanar wings, swept - back wings, variable - geometry wings,shortmoment coupling conad configurtion are indicated. The analysis is focused the advantage of forward - swept wing and triplanar aircraft. A special spread phys technique is introduced, which uses carbon fibre strengthen composite material to perform aeroelasicty cutout, this is key technque conquer fomerd - swept wing aeroelasticty diverge and fulfil forwerd - swept wing plan. |
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| Keywords: | forward-swept wing triplanor aircraft aeroconfiguration aeroelasticity diverge aeroelasticity tailor composite material spread phys technique |
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