Department of Mechanical and Aerospace Engineering University of California Los Angeles, CA 90095-1597;
α: speed of sound; also location of elastic axis; A: wing aspect ratio; c: = 2b = airfoil or wing chord; g: structural damping; h: plunge (bending) displacement at elastic axis (EA), positive down; E_(tot): = T+ U = total energy (structure); k: = ωb/U = reduced frequency; m: mass per unit span; M: Mach number; p: pressure; q: = 1/2ρ_∞U_∞~2, = dynamic pressure; t: time; T: kinetic energy; U-bar: = U_∞/bωα= reduced velocity; U: strain energy; U_∞: freestream velocity at upstream infinity; α: angle;
机译:更好地理解跨音速颤振:三参数颤振曲面
机译:通过LSTM网络对不同马赫数和攻角的跨音颤动边界的高效预测
机译:具有变形装置的翼型的横向颤动特性
机译:非血液跨越扑颤
机译:直接欧拉-拉格朗日方法的曲柄翼的计算跨音速颤振解决方案。
机译:跨音速下高度不规则物体的空气动力学— STRATOS飞行数据分析
机译:具有变形装置的翼型的横向颤动特性