The vibration power flow in a submerged infinite constrained layer damping (CLD) cylindrical shell is studied in the present paper using the wave propagation approach. Dynamic equations of the shell are derived with the Hamilton principle in conjunction with the Donnell shell assumptions. Besides, the pressure field in the fluid is described by the Helmholtz equation and the damping characteristics are considered with the complex modulus method. Then, the shell-fluid coupling dynamic equations are obtained by using the coupling between the shell and the fluid. Vibration power flows inputted to the coupled system and transmitted along the shell axial direction are both studied. Results show that input power flow varies with driving frequency and circumferential mode order, and the constrained damping layer will restrict the exciting force inputting power flow into the shell, especially for a thicker viscoelastic layer, a thicker or stiffer constraining layer (CL), and a higher circumferential mode order. Cut-off frequencies do not exist in the CLD cylindrical shell, so that the exciting force can input power flow into the shell at any frequency and for any circumferential mode order. The power flow transmitted in the CLD cylindrical shell exhibits an exponential decay form along its axial direction, which indicates that the constrained damping layer has a good damping effect, especially at middle or high frequencies.
Vibration Power Flow Analysis of a Submerged Constrained Layer Damping Cylindrical Shell
Contributed by the Design Engineering Division of ASME for publication in the JOURNAL OF VIBRATION AND ACOUSTICS. Manuscript received March 2, 2013; final manuscript received July 20, 2013; published online October 3, 2013. Assoc. Editor: Marco Amabili.
- Views Icon Views
- Share Icon Share
- Search Site
Wang, Y., and Zheng, G. (October 3, 2013). "Vibration Power Flow Analysis of a Submerged Constrained Layer Damping Cylindrical Shell." ASME. J. Vib. Acoust. February 2014; 136(1): 011005. https://doi.org/10.1115/1.4025443
Download citation file: