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Quantifying Intracellular Mechanosensitive Response upon Spatially Defined Mechano-Chemical Triggering

Zare-Eelanjegh E, Lewis RT, Lüchtefeld I, Kutay U, Zambelli T.   +4 more
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Vibration analysis of cylindrical panels

Journal of Sound and Vibration, 1972
Abstract The finite strip solution for the free vibrations of cylindrical panels with any homogeneous boundary conditions is presented. The effects on the natural frequencies for different parameters such as radius, thickness and Poisson's ratio are studied and the numerical results are compared with other exact and approximate solutions.
Cheung, YK, Cheung, MS
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Nonlinear Buckling and Stability of Cylindrical Panels

SIAM Journal on Mathematical Analysis, 1979
The problem of the buckling of a simply supported thin, elastic, cylindrical panel subjected to a uniform axial compression is studied by constructive methods. In the case of “narrow” panels we obtain near the classical buckling load $\lambda _1 $ a description of all stable and unstable buckled states which branch from the unbuckled state at $\lambda ...
Knightly, George H., Sather, D.
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Elasticity solution for laminated anisotropic cylindrical panels in cylindrical bending

Composite Structures, 1995
Abstract This paper establishes the three-dimensional elasticity solution for infinitely long, arbitrarily laminated, anisotropic cylindrical panels with simply supported boundary condition under transverse loading. Using a series method, the solution can be formulated exactly.
Hung-Sying Jing, Kuan-Goang Tzeng
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Edge debonding in patched cylindrical panels

International Journal of Solids and Structures, 1996
Abstract Circumferential edge debonding is considered for structural configurations corresponding to patched cylindrical panels, under a variety of loading conditions. These include applied circumferential tension, radial three-point loading, and applied pressure.
Bottega, W. J., Loia, M. A.
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Some aspects of cylindrical shell panel flutter

5th Aerospace Sciences Meeting, 1967
Abstract : The investigation makes a direct comparison of cylindrical shell panel flutter boundaries obtained analytically with recent experimental boundaries reported in the literature. Further, an attempt was made to explain the discrepancies of the comparison through refinements of some structural aspects of the analysis.
Carter, L. L., Stearman, R. O.
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Natural vibrations of parallelogram cylindrical panels

Strength of Materials, 1981
In the present study, the problem of the natural vibrations of cylindrical panels restrained along the entire perimeter is examined in the linear statement. The solution of this problem presents significant difficulties caused by the skew edges of the panels.
E. S. Belyanovskii, V. A. Pukhlii
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Free Vibrations of Oval Cylindrical Panels

Journal of Engineering Mechanics, 1984
In this paper the dynamic characteristics of oval cylindrical panels, with simply supported curved edges and various boundary conditions along the straight edges, are established on the basis of the Flugge or Donnell type theories using the procedure presented by the writers (5).
Vlasis K. Koumousis, Anthony E. Armenàkas   +1 more
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