摘要
从飞行力学分析的角度 ,用传统的气动力估算方式对具有倒“Y”型尾翼的系缆气球的气动力特性进行估算 .考虑气球与系缆的综合系统 ,建立系缆气球平衡方程并进行配平计算 .在不同的风速条件下 ,采用牛顿下降梯度法迭代求解非线性代数方程组形式的系缆气球平衡方程 .通过不同风速及不同系缆位置的平衡状态的对比分析 。
The aerodynamic characteristics of a tethered balloon with inverted Y fins were estimated by the traditional aerodynamic estimation from the flight dynamics analysis viewpoint. Taking the whole cablebody system into account, the nonlinear force trims equations and nonlinear moment trim equations were established and calculated. For different wind speed, the equilibrium points could be got from the trim equations by Newton iteration method. Comparing the trim states of different wind speed and different junction point of cable, the better junction point of the rope could be confirmed.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
2004年第5期419-424,共6页
Journal of Beijing University of Aeronautics and Astronautics
关键词
飞行力学
气动力
气球
倒“Y”型尾翼
配平
Aerodynamics
Cables
Fins (heat exchange)
Flight dynamics
Nonlinear systems