2009
DOI: 10.1007/s10778-009-0209-4
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Experimental studies of the vibrations and dynamic stability of laminated composite shells

Abstract: The paper discusses the results of systematic experimental studies of vibrations and dynamic instability of thin shells of revolution made of laminated composite materials (glassfiber-reinforced plastics). The basic patterns in the dynamic deformation of shells during natural, forced, and parametric vibrations are considered. The damping parameters of natural vibrations are analyzed. The wave deformation modes of shells subject to periodic excitation are studied. The effect of long-term vibratory loading (tors… Show more

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Cited by 21 publications
(25 citation statements)
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“…As is seen, when the amplitude g v is low, the radial vibrations with maximum amplitude 2A of the shell's free end are excited at the resonant frequencies of conjugate modes with wave numbers n = 3, 4 corresponding to the minimum frequencies, which was mentioned earlier [13,16].…”
Section: Experimental Results 21 Deformation Of the Elastic Wall Osupporting
confidence: 58%
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“…As is seen, when the amplitude g v is low, the radial vibrations with maximum amplitude 2A of the shell's free end are excited at the resonant frequencies of conjugate modes with wave numbers n = 3, 4 corresponding to the minimum frequencies, which was mentioned earlier [13,16].…”
Section: Experimental Results 21 Deformation Of the Elastic Wall Osupporting
confidence: 58%
“…If g v = 2-4g 0 , vibrations with n = 3 are excited only in one of the two conjugate modes. As indicated earlier [13,16], the second mode is excited by a vibration load of high amplitude. In the dry shell, the second conjugate mode with n = 3 is excited when g v = 5g 0 .…”
Section: Experimental Results 21 Deformation Of the Elastic Wall Omentioning
confidence: 54%
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“…An analysis of the above results reveals a qualitative difference between the cases of K 0 0 = and K 0 0 ¹ . As follows from (2.4), the former case takes place when u 30 = u 40 = 0, which corresponds to the steady-state dynamic deflection w (1.3) in the form of a standing wave [12] with the axisymmetric term w 11 ¹ and corresponds to a generalized (with variable amplitude and phase) circumferential traveling wave [13,19]. Figure 1a demonstrates that as the external excitation frequency W is slowly varied, the deformation mode of the shell in the resonance zone changes between a standing wave and a traveling wave.…”
Section: Numerical Examplementioning
confidence: 99%