摘要
根据近年来Ｙ７系列飞机的飞行试验数据、风洞实验数据和ＡＨ－２４，ＡＨ－２６飞机的有关原始资料，详细地分析了Ｙ７－２００Ｂ／Ａ飞机的纵、横航向静稳定性。并对飞机的质心后限、“自动上舵”和“蹬舵反倾”等问题进行了充分的分析和论述，提出了解决此类问题的建议，对民机设计工作有一定的参考价值。
The longitudinal,lateral and directional static stability of Y7-200B/A air-craft are detailedly analysed in the flight test,the tunnel test of Y7 seires aircrafts and the in-formation about AH-24,AH-26 aircrafts,And the AFT.CG,“rudder over balance”,“reverse banking due to rudder movement”are analysed and stated. The opinions for solvingthe problems are raised.There are some reference costs for civil aircraft designing.
出处
《飞行力学》
CSCD
北大核心
1995年第4期56-64,共9页
Flight Dynamics
关键词
静稳定性
适航试飞
质心后限
旅客机
操纵性
Static stability Airworthiness flight test AFT. CG Rudder over balance Reverse banking due to rudder movement
