摘要
本文主要描述在 FL-1风洞中进行的全动翼铰链力矩实验,研究了不同滚转角及不同相邻翼面偏角对压心位置和铰链力矩的影响。
This paper mainly describes the experimental techniqueof all-moving wing hinge moment and data processing in FL-1 windtunnel,and investigate the effects of different roll angle and wing-planedeflective angle on pressure centre position and hinge moment.
关键词
全动翼
铰链力矩
风洞实验
exprimental technique
all-moving wing
hinge moment
