Effectiveness of flexible and rigid ring baffles for damping liquid oscillations in large-scale cylindrical tanks
Effectiveness of lightweight flexible and rigid ring baffles for damping liquid oscillations in large scale cylindrical tanks
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Effectiveness of lightweight flexible and rigid ring baffles for damping liquid oscillations in large scale cylindrical tanks
Passive damping method for aligning instantaneous spin, symmetry, and angular momentum axes of solid axisymmetric almost spherical satellite gyroscope
Joint damping of scaled cantilever beams
Mathematical model for representing restoring force in hereditary springs showing hysteretic damping
Validity of wave damping computation for viscous liquid of finite depth
Vibration frequency and damping behavior of Stored Tubular Expendable Member /STEM/ booms
Analytical representation of damping forces for missile design
Frequency and viscous damping of liquids during weightlessness - liquid sloshing characteristics of liquid-vapor interface in zero Bond number environment
Physical characteristics arising during damping of shock waves in nonuniform media
Model scale effect on structural joint damping
Aerodynamic damping coefficient from wind tunnel free flight trajectories of nonaxisymmetrical bodies
Free vibration and damping of thin walled cylinders
Landau damping and growth applied to electron plasma waves for Maxwellian velocity distribution in slab and cylindrical geometries
Individual section dampers relation to modal damping of series mass spring in lumped parameter systems
Stability of equilibrium of nonconservative continuous systems with slight damping
Cyclotron harmonic wave propagation in warm magnetoplasmas predicted theoretically for perpendicular and oblique damping
A wind-tunnel investigation has been made at low speed to determine the effects of vertical fins placed ahead of the vertical tail on the directional stability and damping-in-yaw characteristics of a swept-wing model under steady-state oscillatory conditions. Various sizes of fins were used above and below the fuselage center line. The vertical-tail size also was varied.