B II! D 50 mm 700 N.m 20 mm ..... 十十 30 mm I П-П Кesiti 200 mm 400 mm 300 mm I-I Kesiti

Q: The beams described in the problems for Section 9.9 have constant flexural rigidity El. A simple…

A: Take a section xx at x distance from A

Q: Please explain all question and draw diagram

A: Part 1. Calculate the displacements at the jointsGiven InformationThe truss structure is square with…

Q: Please show me how to solve this with the stiffness method

A: Calculate the angle:tan∅=34tan∅==36.87°Degree of freedom =5No degree of freedom at joint 1 due to…

Q: Shafts A and Bare made of the same material and have the same cross-sectional area, but A has a…

A: Given:The shafts A and B are having same cross-sectional area According to the problem statement, we…

Q: A B LAB a C D LCD Rigid element b E

A:

Q: For the truss shown in the following figure, the temperature of member BC is raised by 140 °C, and…

A:

Q: Problem 1 A bar obtained by bonding together pieces of aluminum (E, = 70 GPa) and brass (E, = 105…

A: We have to determine the value of largest moment M that can be applied about the horizontal axis…

Q: Refer image below

A: Given data: Steel:L=2 mDi=70 mmDe=100 mmBronze:L=1.5 mD=70 mm

Q: a. The beam weighs 3600N. Draw the V and M diagram. b. Assume we do not know the weight of the beam…

A: 1-If Beam weighs 3600 N then drawing of SFD and BMD2- if Beam Weighs is not know then finding of…

Q: Pin-connected rigid bars AB, BC, and CD are initially held in the positions shown by taut wires (1)…

A: Strain is the result of a material's deformation due to stress. It's only a proportion of the length…

Q: When force P is applied to the rigid arm ABC, point B displaces vertically downward through a…

A: To find the normal strain in wire CD, we need to determine the elongation of wire CD caused by the…

Design of structures using FEA

An arrangement, in which various members are interconnected with their constrained relative motion, the whole arrangement is then known as a structure. The degree of freedom of such a structure is zero. In such a structure, the load can act throughout the length of the structure or at the joints.