Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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A simply supported beam 4 m long has a cross section shown. Determine the maximum uniformly distributed load which can be applied over the entire length of the beam if the shearing stress is limited to 1.7 MPa. Answer must be in kN/m. Given: b= 130 mm and d = 160 mm.
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- The internal shear force V at a certain section of an aluminum beam is 11.4 kN. If the beam has the cross section shown (assume a=39 mm, bf=88 mm, tw=t₁=4 mm, d=71 mm), determine: (a) the shear stress T at point H, which is located 39 mm above the bottom surface of the tee shape. (b) the maximum horizontal shear stress Tmax in the tee shape. a H Answers: (a) TH (b) Tmax= = bf V d MPa. MPa.arrow_forward3. Solve the following problem The following shaft is subjected to three torsional moments expressed as a fraction of T. Determine the maximum value of the T if the allowable shear stress is Tallow 80 MPa. Draw the torsion (torque) diagram along the shaft for that value of T, and determine the relative angle of twist between sections A and C (use a shear modulus G = 26GPa). = diameter d 60mm Tallow 80MPa G = 26 GP₂ Req'd: allowable torque T angle of twist of A relative to C PAIC Torsion diagram 1.2m 1.2marrow_forwardAnswer in two decimal places pleasearrow_forward
- The beam is subjected to the load at its end. Take P=4.2 kN and V = 2 kN. (Figure 1) Figure 1 of 1 30 mm VV 60 mm 2m B The beam is subjected to the load at its end. Take P = 4.2 kN and V = 2 kN .Determine the maximum principal stress at point B.arrow_forward1000 N/m Given: A cantilever beam has loading and cross section as shown. The allowable stress is 64 MPa. 150 mm Determine: the minimum width for the beam 6 m barrow_forward1.8arrow_forward
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