The simply supported beam is comprised of a W24x55 wide flange shape with a pin support at "A" and a roller support at "B" (See text Table A3 for W24 properties) 1. Draw shear and moment diagrams for the beam loaded as shown 2. Determine the maximum bending stress in the beam cross section 3. Determine the maximum horizontal shearing stress in the beam cross section P=14 K 6 K/FT В AL А W24x55 10' 3' 5' RA RB

The simply supported beam is comprised of a W24x55 wide flange shape with a pin support at "A" and a roller support at "B" (See text Table A3 for W24 properties) 1. Draw shear and moment diagrams for the beam loaded as shown 2. Determine the maximum bending stress in the beam cross section 3. Determine the maximum horizontal shearing stress in the beam cross section P=14 K 6 K/FT В AL А W24x55 10' 3' 5' RA RB

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

Two 160 mm * t cover plates are welded to two cahnnels 200 mm high to form the cross section of the beam shown in the figure. The moment of inertia of each channel about a horizontal axis through the centroid is 2.06*106mm4. a)Determine the support reactions. b)Draw the shear force and bending moment diagrams. c)If the allowable bending stress of the beam is 255 MPa, find the required thickness t of the plates to safely support the load.
calculate the location of the centroid, the second moments and product of area for the cross- section if; D = 67 mm, B = 41 mm & t = 2.41 mm A L Test beam A Strain gauge W (a) Unsymmetrical cantilever beam with weight applied at the free end and at the "shear centre", so that there is no torsion induced. Section A-A Strain gauge 1 Strain gauge 2 b Strain gauge 3 a B (b) Location of Huggenberger strain gauges From these, calculate the orientation and position of neutral axis for pure bending in the vertical plane (i.e. bending about a horizontal axis).
If the beam is subjected to an internal moment of M = 30 kN-m determine the compressive bending stress in MPa on the top surface of top flange A. 50 mm 50 mm 10 mm M 150 mm 15 mm
Questions a/b c₁ = c₂ = c 5 0.291 10 0.312 20 0.323 40 0.328 200 10 E m 200 10 1. 6.3 kNm torque is applied to a 3m long steel angle with a 200mm x 200mm x 10mm cross section. From tabulated properties for equal angles, the gross cross sectional area of the section is 5090 mm². knowing that G = 77 GPa, determine (a) the maximum shearing stress along line m-m. Provide the answer in MPa with precision n to two decimal points. 2. Determine the angle of twist if 1.7 kNm of torque is applied to the above long angle steel. Provide the answer in Degrees with precision to two decimal points.
The rigid bar ABC shown is hinged at A and supported by a steel rod at B. FAH 2m 25KN FAV What is the shear force at A in N?
The cross-sectional area of each member of the truss is 1.6 in2. Calculate the average normal stresses in members CE. D. 6 ft B F 8 ft 8 ft E 8 ft 6 ft 30 kips 6.833ksi O 6.250ksi O 10.417ksi O 9.362ksi
The beam shown below is supported by a pin at A and a short link BC. Determine the maximum magnitude P of the loads the beam will support if the average shear stress in each pin is not exceed 80 MPa. All pins are in double shear and have a diameter of 18 mm. 2P 2P 1.5
Problem 4: A high-strength steel wire CD is restraining an angle bracket ABC which supports a load P at A. Diameter of wire CD is 1/8 of an inch and the diameter of the pin at B is 1/8 of an inch. Determine the tensile stress in wire CD and the direct shear stress in the pin at B. 150 P=300lb. -5 in- dw ↓ 1 4 in. D View a-a of B
A horizontal beam AD is supported by an inclined strut BC carries a load W = 2.4KN at the position shown. The strut, which consist of one bar is connected to the beam by a bolt passing through the three bars meeting at joint C. BC is 75mm wide x 10mm thick strut while AD is 100mm wide by 10mm thick rigid bar. a. Determine the required bolt diameter at A if the allowable bolt shear stress is 68MPA, assuming single shear. b. Determine the total vertical displacement at D if E = 200,000MPa A C 10 10 1.2 B Joint at C 1.2 1.2
Week 5, Question 2: Using the force method, calculate the bending moment at B for the statically indeterminate frame below. Please ignore the axial and shear deformations. Take a 12 kN and L = 5.5 m. a B EI A 2EI -3 m Calculate the bending moment at B: kN m MB 2EI m D EI E +=+ L
Beam AB is supported as shown in the figure. Tie rod (1) is attached at B and C with double shear pin connections, while the pin at A is attached with a single shear connection. The pins at A, B, and C each have an ultimate shear strength of 57 ksi, and tie rod (1) has a yield strength of 33 ksi. A concentrated load of P = 14 kips is applied to the beam as shown. A factor of safety of 2.4 is required for all components. Determine: (a) the minimum required diameter for tie rod (1). (b) the minimum required diameter for the double shear pins at B and C. (c) the minimum required diameter for the single shear pin at A. 6.7 8 in. 3.8ft (2) 8.5ft
At a point 8ft from D, solve the shear stress 4in from the top of the cross-section. The cross section is 6in by 18in. 16 k 2 k/ft 8k 3 k/ft B -12 ft 8 ft-+9 ft- 12 ft +-9 ft- 4 ft 3 ft 3 ft O 16.46psi O 65.84psi O 8.23psi O 32.92psi