Download Active and Passive Vibration Control of Structures by Peter Hagedorn, Gottfried Spelsberg-Korspeter PDF

By Peter Hagedorn, Gottfried Spelsberg-Korspeter

Active and Passive Vibration keep watch over of constructions shape a subject matter of very real curiosity in lots of various fields of engineering, for instance within the car and aerospace undefined, in precision engineering (e.g. in huge telescopes), and likewise in civil engineering. The papers during this quantity compile engineers of alternative heritage, and it fill gaps among structural mechanics, vibrations and glossy keep an eye on concept. additionally hyperlinks among the various functions in structural keep an eye on are shown.

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The correction for higher modes are negligibly small, and can be dropped for all practical purposes. The eigenfunctions for the non-zero eigenfrequencies can be determined from (227)-(230). It can be easily checked that solving for B1 from (227)(229) yields − sinh βn l + sin βn l (234) B1 = B2 := αn B2 . cosh βn l − cos βn l Therefore, taking B2 = 1, a possible solution is given by B1 = α n , B2 = 1, B3 = αn , and B4 = 1, (235) which yields the nth eigenfunctions as − sinh βn l + sin βn l (cosh βn x + cos βn x).

7(b), the boundary condition are w(0, t) ≡ 0, EIw,xx (l, t) ≡ 0, and aw,x (0, t) = w(l, t). The natural boundary condition in this case also can be obtained easily from the boundary terms in (167). (a) Simply supported beam (b) Cantilever beam (c) Beam with a sliding boundary Figure 8: Various boundary conditions for a beam Various Boundary Conditions for a Beam Some of the above boundary conditions are realized in various combinations in beams depending on the support, as illustrated in Fig. 8.

The solutions of the characteristic equation are obtained as β2 = nπ , l n = 1, 2, . . , ∞. (211) Substituting this expression of β2 in (199), and solving for ω yield the circular natural frequencies of a simply-supported uniform Rayleigh beam as ωnR = n2 π 2 l2 1 1+ n2 π 2 I 2 l A 1/2 EI , ρA n = 1, 2, . . , ∞. (212) Taking n 1 such that 1+n2 π 2 I/l2 A ≈ n2 π 2 I/l2 A, one obtains from (212) the approximation ωnR ≈ (nπ/l) E/ρ. As can be easily checked, these are the circular eigenfrequencies of longitudinal vibrations of a fixed-fixed bar.

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