1967
DOI: 10.1016/0020-7403(67)90032-x
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Air and internal damping of thin cantilever beams

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Cited by 90 publications
(39 citation statements)
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“…The effect of aerodynamic damping in the case of flexural beam vibrations was considered by Baker et al [12], Adams and Bacon [2] and Crane and Gillespie [13]. Air damping is due to both air viscosity and inertia effects, and increases with the increase in the amplitude of vibrations.…”
Section: Analysis Of the Frequency Responsementioning
confidence: 98%
See 1 more Smart Citation
“…The effect of aerodynamic damping in the case of flexural beam vibrations was considered by Baker et al [12], Adams and Bacon [2] and Crane and Gillespie [13]. Air damping is due to both air viscosity and inertia effects, and increases with the increase in the amplitude of vibrations.…”
Section: Analysis Of the Frequency Responsementioning
confidence: 98%
“…The beam response w 0 (x,t) can be obtained using a modal analysis of Eq. (12). In the case of a load of amplitude p 1 , concentrated at point xZx 1 of the beam (Fig.…”
Section: Damped Vibrationsmentioning
confidence: 99%
“…al. [10], the auhors have drawn conclusions about air damping contribution from tests at aluminum beam specimens in a cantilever configuration. The trend is (i) that for large bending amplitudes air damping is increasing in proportion to the amplitude and (ii) that for small amplitudes the air damping loss factor appears to approach a limit which is independent of amplitude.…”
Section: Air Dampingmentioning
confidence: 99%
“…Table 3 higher from NExT estimates. This difference was shown to be due to a drag phenomenon similar to that experienced by an oscillating flat-plate normal to a strong wind [16,17]. Reference [7] contains the results of a simplified calculation, which predicts 1.2% added damping due to the aero-drag effects for the first blade flatwise modes.…”
Section: Verification Of Next (Oma) Using Conventional Modal Test Resmentioning
confidence: 99%