摘要
介绍了机身气动载荷垂直平面内和水平平面内的几种典型分布形式,并推导出各分布形式下的计算公式。
This paper introduces several typical distribution forms of aerodynamic load of fuselage in the vertical plane and horizontal plane and infers the calculation expression of each distribution form.
出处
《洪都科技》
2009年第4期9-16,共8页
Hongdu Science and Technology
关键词
气动
平衡
力矩
Aerodynamic Balance Moment of force
