w
1. A simple supported beam AB with 2 ft x2 ft cross section is under the...
oints) The beam shown in the figure below is in supported at A and simple su Q3)(100 points) The b a) Use singularity function ularity functions to find the shear and bending moment equations. singularity functions and find the equations of shear and bending spin supported at A and simple supported at b) Evaluate the singularis segment of the beam. Shear and bending moment as a function of x) for each 20 kN/m -4 m 2m- eace to draw an...
1. For the simply supported beam subjected to the loading shown, Derive equations for the shear force V and the bending moment M for any location in the beam. (Place the origin at point A.) a. b. Plot the shear-force and bending-moment diagrams for the beam using the derived functions c. Report the maximum bending moment and its location. 42 kips 6 kips/ft 10 ft 20 ft
2. A 30 ft long simply supported beam supports a uniformly distributed load of 2 kips/ft over the entire span. The beam and cross section are shown below. Draw the shear and moment diagrams, find the neutral axis location, moment of inertia of the composite section, the maximum bending stress on the cross section. (40 points) 10" 2 k/ft 1-3" 30'-0"
5. (20 Points) For the loading on the simply supported beam shown below. a) What is the internal shear and bending moment at point C? b) Given the beam has a rectangular cross section with a width of 8 in. and a height of 20 in., find the maximum normal stress (om) in the cross section at C from the bending moment calculated above. 600 lb 200 lb/ft
For the simply supported beam subjected to the loading shown, derive equations for the shear force V and the bending moment M for any location in the beam. (Place the origin at point A.) Let w = 7.0 kips/ft, a= 9.0 ft, and b= 20.5 ft. Construct the shear-force and bending-moment diagrams on paper and use the results to answer the questions.Calculate the reaction forces By and Cy acting on the beam. Positive values for the reactions are indicated by...
A simply supported beam as shown in the figure. The beam section is W18x211. The beam must support its own weight and must carry the following loading: Super-imposed distributed dead load = 0.25 kip/ft Distributed live load = 1 kip/ft Concentrated dead load = 12 kip The beam span L = 26 ft and the distance of the concentrated load from the right support a=6 ft. Consider analy- sis of beam subjected to load combination 1.2 dead + 1.6 live....
The beam has the rectangular cross section shown. A beam of length 6 meters pin-supported 2 meters from the left end and roller-supported 2 meters from the right end. The beam has a rectangular cross section with base length 50 millimeters and height 150 millimeters. Load: w, uniform along beam. Part A If w = 4 kN/m , determine the maximum bending stress in the beam. Can you please draw out the moment and shear diagrams for this one using...
a simply supported beam abcd with arectangular cross section carries the loading shown in figure. the uniform beam has a mass of 33 kg per meter (m kg/m) and a cross section as shown in the figure. you may take 10 m/s^2 as acceleration.Question A2 A simply supported beam ABCD with a rectangular cross-section carries the loading shown in Figure QA2. The uniform beam has a mass of m kg per meter of length (m kg/m) and a cross-section as shown...
2. (30 pts) The framework consists of three A-36 steel beams AB, CD, and BC. Each beam has a flexural rigidity EI (kip-ft?). The loading condition is shown in the figure below. (note: beams AB and CD are cantilevered beams subjected to uniform loads 5 kip/ft for 8 ft. Beam BC is a simple supported beam subjected to a force 15 kip in the middle of the beam). Appendix C of deflection charts is on the textbook. a) Calculate the...
Assume a beam has the loading shown and a rectangular cross section. is at the center and G is at the bottom. Assume point E is at the top, F Cross Sectional View of plane cut at B 400 lb 4 in 500 lb 3 in 10 in. 15 it 1 5 in 1) The beam is cut along a face at B that is perpendicular to the X axis. What is the internal resistive shear force at this face?...