A change in plate thickness reduces the flutter load drastically.
计算表明厚度的微小变化会引起颤振载荷明显的减小。
Experiment results also reveal that stiffened thin-walled composite plate can bear greater load after buckling. And buckling mode change after stringer adhesive fails.
试验还发现复合材料薄壁加筋板结构有较高的后屈曲承载能力，后屈曲过程中由于桁条脱胶会造成屈曲模态的变化。
应用推荐