Page 43 - Failure Analysis Case Studies II
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                        7.  Wood, R. H., Engineering Plasticity, Cambridge University Press, 1968.
                        8. Jones, N.,  Report 71-20, contract GK-20189X, 1971.
                        9.  Hodge, P. G., Limil Analysis of  Rotationally Symmetric Plales and Shells. Prentice-Hall,  1963.
                       IO. Wood, R. H., Plastic and Ehtir I)e.sign of  Slabs and Plates. Ronald Press, 1961.
                       11.  Johnson, R. P.. Structural Concrete. McGraw-Hill, 1967.


                                                        APPENDIX
                       Estimafe of  Iowest nalura1frequenc.v offirewalf segment
                         An upper bound to the lowest natural frequency w of a plate with all edges clamped, uniform mass per unit area m and
                       uniform plate flexural rigidity D, can be estimated by Rayleigh's method from




                       where w(x,  y) is a arbitrary deflection function which satisfies the kinematic boundary conditions, and both integrals are
                       over the area of the plate. We consider a triangular plate whose vertices are (0, 0) (a, 0) and (0, h), and take



                       which satisfies the boundary conditions for a clamped plate. The calculation is assisted by the integral




                       which is a special case of a standard integral quoted by Gradshteyn and Ryzhik 151. After some algebra:
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