A beam and it's cross-section is given in the figure. Point A is fixed, point B is rollersupported. Also, there is a hinge at point G of the beam. Calculate the maximum tensionOma,tension (MPa) and maximum compression oma compression (MPa) for the cross-section.Note: Centroid of the section is 120 mm above from the bottom fiber.P(7kNyAq(2kN/m)150 mmABG'hingeL-2m4 m2 m30, mmBeam sectionResults TableOmax, tension (MPa)=Omax,compression (MPa)=j=120ww150 mm180 mmwwos

A beam and it's cross-section is given in the figure. Point A is fixed, point B is roller supported. Also, there is a hinge at point G of the beam Calculate the maximum tension Oma (MPa) and maximum compression oma.compresion (MPa) for the cross-section. tension Note: Centroid of the section is 120 mm above from the bottom fiber. P(7kN yA q(2kN/m) 150 mm A G hinge L-2m 4 m 2 m, 30, mm Beam section 180mm ww O wwfos ww

A beam and it's cross-section is given in the figure. Point A is fixed, point B is roller supported. Also, there is a hinge at point G of the beam Calculate the maximum tension Oma (MPa) and maximum compression oma.compresion (MPa) for the cross-section. tension Note: Centroid of the section is 120 mm above from the bottom fiber. P(7kN yA q(2kN/m) 150 mm A G hinge L-2m 4 m 2 m, 30, mm Beam section 180mm ww O wwfos ww

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

Solve correctly
A steel rod is stretched between two walls. At 20°C, the tensile force in the rod is 3000 N. If the stress is not to exceed 150 MPa at -20°C, find the resulting stress in MPa due to change in temperature. Use a= 11.7 x 10-6/°C and E=200 GPa. Answer:
DETERMINE FORCE (N) OF MEMBER EG in the truss shown. F1 = 237 N F2 = 682 N F3 = 456 N α = 40 degree x = 8 m. Note: for compression, include a negative sign ( - ) and for tension, type your answer as is. Input your answer in two (2) decimal places only.
Problem II. An exhaust gas piping fabricated as shown is subjected to a bending moment, an internal pressure, and a torque. In points A and B, the following stresses occur due to the loading: o 63.5 MPa, B=127 MPa, = 127 MPa A.B A.B a. Determine Gmin, omax, and its direction (in degrees) from x-axis at point A. b. Determine omin, omax, and its direction (in degrees) from x-axis at point B. 1 B d O A x
2. Determine the normal stress in members BD, AC, and BC in the truss shown. The cross- sectional area of each member is 1500 mm2. Indicate whether the stresses are tensile (T) or compressive (C). Use 2 decimal places in every solved value. 10 m 10 m 10 m K 6 т H 6 т 15° 15° 50 kN 40 kN E F 6 т C D б т A B
A bronze pipe (1) is to be connected to an aluminum alloy pipe (2) at flange B. When put in place, however, a gap of A = 0.25 in. exists between the two pipes. Bronze pipe (1) has an elastic modulus of E, = 16,000 ksi, a cross-sectional area of A, = 2.83 in.?, and a length of L1 = 6.9 ft. Aluminum alloy pipe (2) has an elastic modulus of E2 = 10,000 ksi, a cross-sectional area of A2 = 1.47 in.2, and a length of L2 = 12.0 ft. If bolts are inserted in the flanges and tightened so that the gap at B is closed, determine: (a) the normal stresses produced in each of the members. (b) the final position of flange B with respect to support A. L2 В (1) Answer: (a) σ1- ksi 02 = ksi (b) OB/A = in.
3 The piece of plastic is originally rectangular. Calculate the shear strain Yxy at corners A and B if the plastic distorts as shown by the dashed lines. 2 mm 300 mm 2 mm D -400 mm- mm, B A 4 mm 72 mm 3 mm X
Determine the normal stress in members BD, AC, and BCin the truss shown. The cross-sectional area of each member is 1500mm2. Indicate whether the stresses are tensile (T) or compressive (C). Use 2 decimal places in every solved value.
Engineering Mechanics DETERMINE THE INTERNAL FORCE OF MEMBER DF FROM THE FIGURE BELOW. Note: for compression, include a negative sign ( - ) and for tension, type answer as is. Use four (4) decimal places during computation and two (2) decimal places for the final answer.
DETERMINE FORCE (N) OF MEMBER EG in the truss shown. F1 = 214 N %D F2 = 876 N %3D F3 = 435 N a = 38 degree X = 15 m. **Note: for compression, include a negative sign (- ) and for tension, type your answer as is. Input your answer in two (2) decimal places only without the unit. В H A C E G F1 F2 F3
An aluminum bar of cross-section 450 ??² is acted upon by the forces as shown in the figure. Determine the total elongation of the bar. Use ? = 70 ???.
answer f3 and p only