Department of Mechanical Engineering Universite de Sherbrooke Sherbrooke, Quebec J1K 2R1 Canada;
D: Cylinder diameter; L: Cylinder length; m_L: Mass per unit length; L-w: Length of exposed model; H: Height of the wind tunnel test section; φ_(rel): Relative phase angle between vortices and motion, corrected; φ_(rel) no: Relative phase angle between vortices and motion, not corrected; △φ_(rel): Relative phase angle correction; V: Velocity; f_n: Cylinder natural frequency; f_s: Vortex shedding frequency; S_c: Scruton number; ζ: Damping ratio; U: Reduced velocity (V/(2πf_Nd)); A: Cylinder envel;
机译:发生涡旋振动的挠性立管的振动相位角和流体动力
机译:振动和水平角对热管启动和过渡区动力学影响的实验研究
机译:一种实验研究,探讨涡流诱导柔性圆柱振动的独立原理的有效性在一系列倾斜角度下的振动
机译:涡旋诱导振动瞬态制度中的相位角:实验测定
机译:低模数气缸经受涡激振动的实验研究。
机译:大倾角下柔性圆柱体的涡激振动
机译:从涡旋诱导的振动和唤醒振动中压电能量收获的实验研究
机译:提升转子随机载荷和振动的理论和实验研究的概念(从瞬态响应数据中识别提升转子系统参数),阶段7-B