Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
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- A propped cantilever steel beam is constructedfrom a W12 x 35 section. The beam isloaded by its self-weight with intensity q. The lengthof the beam is 11.5 ft. Let E = 30,000 ksi.(a) Calculate the reactions at joints A and B.(b) Find the location of zero moment within span AB.(c) Calculate the maximum deflection of the beamand the rotation at joint B.arrow_forwardA cantilever beam AB, loaded by a uniform load and a concentrated load (see figure), is constructed of a channel section. 250 lb 22.5 lb/ft A 5.0 ft 3.0 ft- 0.617 in. 2.269 in. (a) Find the maximum tensile stress o, (in psi) and maximum compressive stress o, (in psi) if the cross section has the dimensions indicated and the moment of inertia about the z-axis (the neutral axis) is I = 3.10 in4. Note: The uniform load represents the weight of the beam. (Use the deformation sign convention.) O, = psi psi (b) Find the maximum value of the concentrated load (in Ib) if the maximum tensile stress cannot exceed 4 ksi and the maximum compressive stress is limited to 18.0 ksi. (Enter the magnitude.) Ib (c) How far from A (in ft) can load P = 250 lb be positioned if the maximum tensile stress cannot exceed 4 ksi and the maximum compressive stress is limited to 18.0 ksi? ftarrow_forwardA cantilever beam AB supports a distributed load of peak intensity g, acting over one-half of the length (see figure). (The beam has constant flexural rigidity EI. Use the second-order differential equation of the deflection curve. Enter the magnitudes.) ly 90 A C В L/2- L/2 Derive the equations of the deflection curve for the beam. (Use the following as necessary: qo, L, E, I, x.) Osxs v(x) = sxsL vx) = Also, obtain formulas for the deflections 8, and 8. at points B and C, respectively. (Use the following as necessary: 9,, L, E, I.) 7 160 E·I 11 %0 L3 192 E·Iarrow_forward
- A cantilever beam carries a trapezoidal distributed load ( see figure) . Let wB=2.5 kN/ m, wA= 5.0kN/m, and L = 2.5 m. The beam has a modules E = 300 mm, Use the method of superposition and cases 1 and 8 in Table H-1 to calculate the deflection and rotation at B.arrow_forwardA simply supported beam is loaded with apoint load, as shown in the figure. The beam is a steelwide flange shape (W 12 X 35) in strong axis bending. Calculate the maximum deflection of the beam andthe rotation at joint A if L =10 ft, a = 7 ft, b = 3 ft,and P = 10 kips. Neglect the weight of the beam.arrow_forwardA beam ABC having flexural rigidityEI = 75 kN.m2 is loaded by a force P =800 N atend C and tied down at end A by a wire having axialrigidity EA = 900 kN (see figure).What is the deflection at point C when the loadP is applied?arrow_forward
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