Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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- b) A cylindrical rod AB is made of aluminum is connected at B to a brass qylindrical rod BCD as shown in Figure 8. The shear modulus, G of aluminum rod AB is given by 27 GPa and the brass rod BCD of 39 GPa. The torsional reactions, TA and Ts are located at the ends of A and B, respectively. Given the portion CD of the brass rod is hollow and has an inner diameter of 40 mm, examine the angle of twist at A. 60 mm Tg = 1600 N - m 36 mm TA = 800 N m 250 mm 375 mm A 400 mm Figure 8arrow_forwardThe beams described in the problems for Section 9.9 have constant flexural rigidity El. A simple beam AB of length L is loaded at the lefthand end by a couple of moment M, (see figure). Determine the angle of rotation 6, at support A. (Obtain the solution by determining the strain energy of the beam and then using Castigliano's theorem.) Mo B L PROB. 9.9-1 Step-by-step solution Step 1 of 5 A Length of the simple beam AB = L Couple of moment at A,= M, Angle of rotation at A= 0,arrow_forward*14-88. The state of strain at the point on the leaf of the caster assembly has components of = -400(1o). y = 860(10, and Yay = 375(10*). Use the strain transformation equations to determine the equivalent in-plane strains on an element ariented at an angle of e = 30 counterclockwise from the ariginal position. Sketch the deformed element due to these strains within the x-y plane.arrow_forward
- The static indeterminacy of the structure shown below is G F Hinge. С E B (A)Unstable (B) Stable, determinate (C) Stable, 5th degree indeterminate (D)Stable, 3rd degree indeterminatearrow_forwardSolve using Mohr’s circlearrow_forward10-2. The state of strain at the point on the pin leaf has components of € = 200(106), y = 180(106), and Y xy = -300(10-6). Use the strain transformation equations and determine the equivalent in-plane strains on an element oriented at an angle of 0 = 30° counterclockwise from the original position. Sketch the deformed element due to these strains within the x-y plane. X Prob. 10-2/3arrow_forward
- (b) (5 pt) Draw and properly label a free-body diagram of ring A of the structure shown. Include only relevant information; do not include any information that is not relevant to the free-body diagram. Note: Assume the ring at A is massless. 3 m 3 m wwww kac = 20 N/m 4 m KAB = 30 N/m www. KAD = 40 N/m Barrow_forwardPROBLEM 10-1 GIVEN: THE STATE OF STRAIN AT THE POINT ON THE PIN LEAF HAS COMPONENTS OF = 200(106), e,= 180(10), AND Yay = -300(10).; REQUIRED: USE THE MOHR'S CIRCLE AND DETERMINE THE EQUIVALENT IN-PLANE STRAINS ON AN ELEMENT ORIENTED AT AN ANGLE OF 8 - 30° COUNTER CLOCKWISE FROM THE ORIGINAL POSITION. SKETCH THE DEFORMED ELEMENT DUE TO THESE STRAINS WITHIN THE X-Y PLANE.arrow_forwardA compound beam as shown with a pin at A, a hinge at C, and rollers at B and D,1) Draw all F.B.D.s for your calculation;2) Determine the reactions at A, B and D when the beam is in equlibrium [Hint: 1) ABC part is the independent part and CD is the dependent part of the compound beam. The analysis always starts from the dependent part, then the independent part. 2) Draw the FBD of CD part first.]arrow_forward
- Subject is structural analysis Please show each steps to the question and make it easy for me to understand. Explain the diagramarrow_forwardP El is constant, find the reaction forces. Using the method of consistent deformations EI L 0.75L 2P 2EI 0.75Larrow_forwardI need the answer as soon as possiblearrow_forward
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