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。
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.
出处
《飞行力学》
CSCD
北大核心
1994年第1期28-34,96,共8页
Flight Dynamics
关键词
飞机
起落架
突伸
下沉
Carrier aircraft Landing gear Jump Sink
