期刊
JOURNAL OF AIRCRAFT
卷 48, 期 3, 页码 874-883出版社
AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.C031080
关键词
-
资金
- Directorate For Engineering
- Div Of Civil, Mechanical, & Manufact Inn [1031036] Funding Source: National Science Foundation
The flutter analysis of a swept aircraft wing-store configuration subjected to follower force and undergoing a roll maneuver is presented. Concentrated mass, follower force, and roll angular velocity terms are combined in the governing equations, which are obtained using the Hamilton's variational principle. The wing is modeled from a classical beam theory and incorporates bending-torsion flexibility. Heaviside and Dirac delta functions are used to consider the location and properties of the external mass and the follower force. Also, Peters's unsteady aerodynamic pressure loadings is considered and modified to take into account the effect of the wing sweep angle. The extended Galerkin's method is applied to convert the partial differential equations into a set of ordinary differential equations. Numerical simulations are validated with available published results. Simulation results are presented to show the effects on the wing flutter of the roll angular velocity, sweep angle, follower force, and store mass and its location. Results are indicative of the significant effect of the rigid-body roll angular velocity and the follower force on the wing-store dynamic stability. Furthermore, it is shown that the distances between the wing root and the aircraft center of gravity, acting location of the roll angular velocity, considerably affects the wing-engine flutter speed and frequency.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据