By N.E. Shanmugam, C.M. Wang
A concise evaluate of the latest examine and the way it may be utilized in the sector, with a panel of distinctive editors and a crew of overseas members, this ebook is a useful reference resource. It discusses the modeling of plates for results akin to transverse shear deformation and rotary inertia, meeting of plates in forming thin-walled participants, and altering fabric homes in composite, laminated and functionally graded plates. It contains discussions of contemporary thoughts for linear and nonlinear vibration research and concludes with a hybrid procedure compatible for parameter identity of plated constructions and hydroelastic research of floating plated constructions.
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Extra resources for Analysis and Design of Plated Structures: Volume 2: Dynamics
Transactions, ASME, 79, 1459–1475. H. B. (1964), Transverse vibrations of tapered cantilever beams with end loads. Journal of the Acoustical Society of America, 36, 463–469. H. B. (1968), Transverse vibrations of tapered cantilever beams with end support. Journal of the Acoustical Society of America, 44, 1739–1741. H. B. (1972), Transverse vibrations of double-tapered cantilever beams. Journal of the Acoustical Society of America, 51, 1771–1774. H. B. (1974), Transverse vibrations of double-tapered cantilever beams with end support and with end mass.
Finally, it is worth mentioning the more recent work co-authored by Hamed and Frostig (2005), proposing a beam model that accounts for the crosssection in-plane deformation by ensuring displacement compatibility and stress equilibrium along longitudinal edges joining adjacent walls. The natural frequency values obtained by means of this approach are compared with values yielded by shell FEA performed in a commercial code, for members with several cross-section geometries − good agreement was found in all cases.
70 Similarly to the derivation of Eq. 42), substituting Eqs. 70) produces the equations k11 ... ... k18 C1 0 ... ⋅ ... = ... k 88 C8 0 ... ... 7 for a built-in beam. It can be seen that this useful technique for considering a beam with two subdomains within the length l (viz. a prismatic one and a tapered one) can be extended to several subdomains within the length l, but with an increase in the number of deformation coefficients needed to prescribe the problem and hence in the size of the characteristic equation to be solved.