please answer with complete solution for a rate. ty! A rectangular beam is supported at both ends. It carries two concentrated loads of 190KN, a clockwise moment of 160KN-m,and a uniformly distributed load of 94KN/m. The modulus of elasticity of the beam is 190GPa. Solve the following if thereaction at point B is 333.16666666667KN, upward.BEAM DIMENSION: Width = 120mm, Height = 460mmAlso, DON'T FORGET TO TYPE DOWN THE CORRECT UNITS (IF NEEDED)PPM1m1m1mWhat is the numeric value of C1 (1st Constant)?kN-m?Determine the deflection at midspan.

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Answered: A rectangular beam is supported at both…

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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PROBLEM 6: A 10 m steel wide flange beam is laterally supported. The width of the web if the beam is 700 mm and web thickness is 10 mm. If Fy is equal to 250 MPa, the allowable bending stress is: a. 135 MPa c. 185 MPa b. 165 MPa d. 105 MPa
Problem 4: A T section of a beam is fabricated from 2 - 12 mm x 150 mm steel plates and joined by welding as shown in Figure ST-904. It carries a live load of 6.5 kN/m extending half of its span. Neglect the weight of the beam. T 12 x 150 mm 4 m 6.5 kN/m 4 m Compute the maximum compressive stress. ( bending stress in compression) Compute the maximum tensile stress. ( bending stress in tension) Compute the maximum shear stress. Compute the shear stress between the junction of web and flange. Compute the maximum deflection. El is constant.
Two beams of equal lengths are placed on top of the other and carrya total moment of 7 kN-m. The bottom beam is 600 mm by 150 mm and the top beam is 300 mm by 75 mm. Both beams are of the same material and length of 6 m. The modulus of elasticity is 80,000 MPa. Assume the beams are frictionless at the interface. Determine the moment carried by the lower and upper beam, and the maximum flexural stress.
02: The rigid platform has negligible mass and rests on two steel bars, each 250.00 mm long. The center bar is aluminum and 249.90 mm long. Compute the stress in the aluminum bar after the center load P= 400 kN has been applied. For each steel bar, the area is 1200 mm2 and E= 200 GPa. For the aluminum bar, the area is 2400 mm2 and E 70 GPa Rigid platform Steel Ahmum Steel
Given a rectangular hollow box with outer dimensions 125mm x 85mm and constant thickness of 10mm has an ultimate stress of 415 MPa. Modulus of Elasticity of 110 GPa. a. Determine the bending moment M for which the factor of safety will be 2.50. b. Determine the corresponding radius of curvature of the section.
This is a mechanics of deformable bodies problem
QUESTION: The distributed load on the T-section beam shown below and moment affects. A is the fixed joint and B is the sliding joint. This beam is made of a ductile material with a yield stress (σak) of 1000 MPa. The thickness (depth) of the beam profile is t=6 mm. A) As a mechanical engineer, check the strength of this beam (in terms of Normal and Shear Stress) ? B) In order for the existing beam to run smoothly, two 100x25 mm plates made of the same material are planned to be welded to this beam. The mechanical engineer working in the factory told the welder to weld this piece under the beam (where the B point is). But the welder, regardless of what the mechanical engineer said, welded this plate to both sides of the existing T-section beam as shown below, thinking that it wouldn't matter anyway. As a mechanical engineer : 1) After welding these plates on both sides of the beam, as the welder did, find out whether the new beam will work smoothly or not by making the necessary…
H.W 2 A steel tee shape is used to support the loads shown on the beam in Figure 2 a. dimensions of the shape are shown in Figure 2 b. determine: (a) the maximum tension bending stress at any location along the beam, and (b) the maximum compression bending stress at any location along the beam. The Consider the entire 24-ft length of the beam and 16.00 in. y 7 kips 16 kips 17 kips 1.50 in. 6 kips/ft 18.50 in. В C E 6 ft 4 ft 10 ft 4 ft 0.75 in. FIGURE 2 a. FIGURE 2 b.
6-121 A wood beam is reinforced with steel straps at its top and bottom as shown. Determine the maximum bending stress developed in the wood and steel if the beam is sub- jected to a bending moment of M 5 kN m. Sketch the stress distribution acting over the cross section. Take E,, = 11 GPa, Est 200 GPa. 20 mm 300 mm -M = 5 kN-m 200 mm Prob. 6-121 20 mm
A simply supported wood beam AB with span length L carries a uniform load of intensity q kN/m . The elastic modulus of the beam E=10Gpa=109N/m2; L=4m , q=8 kN/m, b=0.1m, h=0.5m . Calculate the maximum bending stress σmax and maximum bending strain εmax due to the load q. Note: the moment of inertia of the cross-sectional area I =bh3/12.
The beam is loaded by two point forces P. The beam is assembled according to the cross-sectional view by nailing wooden parts with cross-sections of 50 mm x c = 220 mm and 25 mm x d = 260 mm. How large can the value of the load P be when the distance between the nails in the longitudinal direction of the beam is 100 mm, the cross-sectional area of the nail is 9 mm2 and their permissible shear stress is 110MPa? Then calculate the maximum stresses and shear stresses of the beam at that load when the distance between the articulated supports is L = 1.9 m and the length of the beam projections a = 1.3 m. Permissible shear force of one nail? kN Static torque of the cutting surface? mm^3 Maximum torque change in cantilever? kNm Cutting force of the projection? kN Magnitude of force P? kN Calculated with the obtained force P maximum normal stress? MPa shear stress maximum? MPa
A wooden beam AB supporting two concentrated loads P has a rectangular cross section of width b = 100 mm and height h = 150 %3D mm. The distance from each end of the beam to the nearest load is a = 0.5 m. The span of the beam is 5 m. Determine the maximum permissible value P (in kN) if the allowable stress in bending is 11 MPa (for both tension and compression). A.

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