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The aerodynamic component of the damping of cantilevered test specimens oscillating near a rigid shield dependence of the logarithmic decrement of oscillations, which determines the damping properties of the test
Theoretical-experimental method of determining the drag coefficient of a harmonically oscillating thin plate coefficient on the basis of the experimentally found logarithmic decrement of beam oscillations.
Theoretical-experimental method of determining the drag coefficient of a harmonically oscillating thin plate coefficient on the basis of the experimentally found logarithmic decrement of beam oscillations.
Theoretical-experimental method for determination of aerodynamic damping component of test samples with diamond-shaped cross-section the lowest experimental frequency and amplitude dependences of the logarithmic decrement which are used
Theoretical-experimental method for determination of aerodynamic damping component of test samples with diamond-shaped cross-section the lowest experimental frequency and amplitude dependences of the logarithmic decrement which are used
Influence of the handle design on a composite lathe cutterlogarithmic decrement
Modeling the Dynamic Response of a Carbon-Fiber-Reinforced Plate at Resonant Vibrations Considering the Internal Friction in the Material and the External Aerodynamic Damping are determined by the logarithmic decrement, which depends on the vibration amplitude of its free edge. Numerical
Evaluation of aerodynamic forces acting on oscillating cantilever beams based on the study of the damped flexural vibration of aluminium test samples is presented based on analysis of experimental measurements of a logarithmic decrement of vibrations
Modeling the Dynamic Response of a Carbon-Fiber-Reinforced Plate at Resonant Vibrations Considering the Internal Friction in the Material and the External Aerodynamic Damping are determined by the logarithmic decrement, which depends on the vibration amplitude of its free edge. Numerical
On the interaction of composite plate having a vibration-absorbing covering with incident acoustic wave logarithmic decrement. Aero-hydrodynamical interaction between plate and external acoustic environment
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