Fighter aircraft; Aircraft maintenance; Tail assemblies; Aeroelasticity; Buffeting; Tails(Aircraft); Mathematical models; Coupling(Interaction); Methodology; Vibration; High rate; Fatigue life; Performance(Engineering); Dynamics; Parameters; Structural properties; Acceleration; Excitation; Reliability; Nonlinear systems; Attack aircraft; Flight envelope; Assembly; Amplitude; Fins; Structural components; High angles; Structural engineering; Variable pressure; Parametric devices; F-15 aircraft; Twin tail aircraft; Buffet; Multi-valued responses; Nonlinear dynamics;
机译:主动涡流控制减轻通用战斗机的双尾自助餐
机译:飞机抖振负荷减轻应用智能鳍模型的主动控制
机译:飞机垂直鳍自助式减轻负荷混合动力系统的主动控制
机译:流量控制减轻双尾自助餐的有效性
机译:双尾战斗机的结构识别和自助减轻。
机译:设计均匀的FeTiO3组件该组件由能够实现高性能准固态钠离子电容器的纳米微粒组成
机译:使用压电式执行器减轻高性能双尾飞机尾部自助