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resonance (natural) frequency of a cantilever beam is given by
f=[kn/2pi][sqrt(EI/wL^4)] where, kn=3.52 for mode 1, E is Young's modulus, I is moment of Inertia, w is beam width, L is beam length. (this is from Formulas for Stress and Strain, 5th edition by Raymond J. Roark and Warren C. Young).
I would like to derive this formula. Can any one suugest me any book or any link?
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