| EXPERIMENTAL RESEARCH OF THE CONFIGURATION OF WING－TIP DRAG REDUCTION FOR LIGHT AIRCRAFT |
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| 引用本文： | Deng Yanmin,HuJizhong(Faculty of Light Aircraft Design,Fifth Dept,Beijing University of Aeronautics and Astronautics,Beijing,China,100083). EXPERIMENTAL RESEARCH OF THE CONFIGURATION OF WING－TIP DRAG REDUCTION FOR LIGHT AIRCRAFT[J]. 中国航空学报, 1994, 0(4) |
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| 作者姓名： | Deng Yanmin HuJizhong(Faculty of Light Aircraft Design Fifth Dept Beijing University of Aeronautics and Astronautics Beijing China 100083) |
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| 作者单位： | Faculty of Light Aircraft Design，Fifth Dept，Beijing University of Aeronautics and Astronautics，Beijing，China，100083 |
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| 摘 要： | ＥＸＰＥＲＩＭＥＮＴＡＬＲＥＳＥＡＲＣＨＯＦＴＨＥＣＯＮＦＩＧＵＲＡＴＩＯＮＯＦＷＩＮＧ－ＴＩＰＤＲＡＧＲＥＤＵＣＴＩＯＮＦＯＲＬＩＧＨＴＡＩＲＣＲＡＦＴＤｅｎｇＹａｎｍｉｎ，ＨｕＪｉｚｈｏｎｇ（ＦａｃｕｌｔｙｏｆＬｉｇｈｔＡｉｒｃｒａｆｔＤｅｓｉｇ...
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EXPERIMENTAL RESEARCH OF THECONFIGURATION OF WING-TIPDRAG REDUCTION FOR LIGHT AIRCRAFT |
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| Deng Yanmin,HuJizhong. EXPERIMENTAL RESEARCH OF THECONFIGURATION OF WING-TIPDRAG REDUCTION FOR LIGHT AIRCRAFT[J]. Chinese Journal of Aeronautics, 1994, 0(4) |
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| Authors: | Deng Yanmin HuJizhong |
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| Abstract: | |
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| Keywords: | light aircraft wing tips drag reduction wind tunnel tests |
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