重心位置对不同布局飞机尾旋特性的影响  

Effect of C.G. Location on Spin Characteristics of Different Layout Aircraft

作　　者：颜巍[1] 黄灵恩 YAN Wei;HUANG Ling'en(Shanghai Aircraft Design and Research Institute,Shanghai 201210,China)

机构地区：[1]上海飞机设计研究院,上海201210

出　　处：《民用飞机设计与研究》2018年第4期29-35,共7页Civil Aircraft Design & Research

摘　　要：为了研究某大型民机重心位置轴向变化对其尾旋特性的影响,在尾旋风洞中进行了飞机模型的尾旋特性研究试验,试验结果表明在前重心条件下,模型旋转更加明显,尾旋情况更为严酷。同时展示了重心位置轴向变化对鸭式布局飞机和高平尾尾吊发动机布局飞机的影响,并进行了对比分析。此外,还研究了重心位置横向变化对常规布局大型民用飞机尾旋特性的影响。An aircraft model was tested in spin tunnel to investigate the effect of C.G.(center of gravity)location in longitudinal direction on aircraft spin characteristics.The results show that the more obvious the model rotates,the more critical spin situation gets under forward C.G.condition.Meanwhile,the effect of C.G.location in longitudinal direction on spin characteristics of canard aircraft and high-tail aircraft are also presented,compared and analyzed.Furthermore,the effect of C.G.location in lateral direction on general aircraft spins characteristics was also investigated in spin tunnel tests.

关 键 词：重心位置 尾旋特性 鸭式布局飞机 高平尾尾吊发动机布局飞机 常规布局飞机 

分 类 号：V212.12[航空宇航科学与技术—航空宇航推进理论与工程]