| 前起落架突伸对舰载机起飞特性的影响 |
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| 引用本文： | 胡淑玲,林国锋.前起落架突伸对舰载机起飞特性的影响[J].飞行力学,1994,12(1):28-34,96. |
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| 作者姓名： | 胡淑玲 林国锋 |
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| 作者单位： | 西北工业大学 |
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| 摘 要： | 研究了前起落架突伸的实现模式和突伸对舰载机起飞特性的影响，分别对四种突伸模式及突伸机构设计参数的作用进行了比较分析，结果表明，前起落架突伸对于减少舰载机离舰后的下沉和缩短飞机起飞滑跑距离有明显的作用。
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| 关 键 词： | 飞机 起落架 突伸 下沉 |
THE EFFECTS OF NOSE LANDING GEARJUMP ON THE CARRIER AIRCRAFT CATAPULT TAKE-OFF FLIGHT PATH |
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| Hu Shuling,Lin Guofeng.THE EFFECTS OF NOSE LANDING GEARJUMP ON THE CARRIER AIRCRAFT CATAPULT TAKE-OFF FLIGHT PATH[J].Flight Dynamics,1994,12(1):28-34,96. |
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| Authors: | Hu Shuling Lin Guofeng |
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| Institution: | Northwestern Polytechnieal University |
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| Abstract: | The models of nose landing gear jump and its effects on the performanceof carrier aircraft during catapult take-off phase have been studied in this paper.Fourmodels of jump and the function of structure projected coefficients have been analyzed.Ithas been concluded that nose landing gear jump has important effects on decreasing thesinkage and take-off distance. |
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| Keywords: | Carrier aircraft Landing gear Jump Sink |
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