Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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The beam AB is subjected to the uniformly distributed load shown and to two unknown forces P and Q. Knowing that it has been experimentally determined that the bending moment is +6.10 kip ft at D and +5.50 kip ft at E, (a) determine P and Q, (b) draw the shear and bending-moment diagrams for the beam. 250 lb/ft C D E F Fig. P7.91
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- 4149 Daternm 4.150 Determine the forces in members BC, BG, and FG.arrow_forwardQ.3) (a) Find the support reactions of the beam shown below. (b) Write the expressions for shear-force (V) and bending-moment (M) for a beam section between points C and D, as a function of x measured from the left-end support. 12 kN 6 kN 4 m 1 kN/m 2 kN/m D 1.5 kN/m 6 m A 1 m 2 m C 30% 3 m 20 kN.m B Aarrow_forwardFor the beam shown, determine the maximum positive and negative shears and the maximum positive and negative bending moments at point C due to concentrated live load of 150 kN, a uniformly distributed live load of 50 kN/m. The weight of the beam is 25kN/m. 5 m 6 m D m 4 m-arrow_forward
- A 60 kN 7.2 m Figure no. 7 B Carrow_forwardThe dead-weight loading along the centerline of the airplane wing is shown. If the wing is fixed to the fuselage at A, determine the reactions at A, and then draw the shear and moment diagram for the wing. 15 kN 6 kN/m 3.75 kN/m- 0,6 m -2.4 m -0.9 m- 75 kNarrow_forward
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