Make normal effort, shear stress and bending moment diagrams, like in the example above. Examples Diagrams[kN]Normal Effort7030[kN]Shear Stress2 m2 m-70[kN.m]Bending Moment100122,5 20321,5Given data:Moment of inertia of the cross section = |Material modulus of elasticity = ECross-sectional area of the bars = AE = 2,05 x 10$ kN/m*; I = 2,083 x 10-3 m*; A = 0,10 m.

Answered: Image /qna-images/answer/31b465cf-b7b9-48e6-9c7c-922bd51d5544.jpg

Answered: Make normal effort, shear stress and…

Engineering

Civil Engineering

Make normal effort, shear stress and bending moment diagrams, like in the example above.

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

Subject : solid Mechanics
2. Maximum tensile and compressive bending stress, Make W= 8 kN/m all dimensions are in mm make answer rounded off into 3 decimal places.
Q1: If the beam with T section shown in Figure I is subjected to a positive bending moment 105 N.m . determine the following: 1. The location of the centroid measured from the top fiber in (mm) 2. The moment of inertia about the centroidal x axis (mm) 3. The maximum compressive stress in (MPa) 4. The maximum tensile stress in (MPa)
Problem 3 For the shown beam. (1) Plot V and M diagram (2) Find the maximum tensile and compressive flexural stresses in the beam and indicate the location (both on beam and cross-sectional area) 2 in. 2 in. 2 in. 2000 lb 800 lb/ft 4000 1b ft B 6 in. 2 in. 3 ft 10 ft 2 ft- (a) (b)
For the beam in figure 1, find the value and location of the largest tensile and compressive stresses. There may be more than one candidate location for each of these. 3.2 kN/m 2 1.9 kN.m Im A 3m 2m Figure 1 Figure 2 The cross section shown in Figure 2 is 125x75x8 UA the cross section and material properties are shown below; (Note that in the tables, the horizontal and vertical coordinate n and p, and are right and up respectively. Table 26 Unequal Angles - x-axis and y-axis - Dimensions and Properties Designation Nominal Mass Actual Radii Thickness per Thickness About x-axis About y-axis Torsion Tan Designation Constant Alpha Gross Coordinate metre Area of of Centroid Cross Leg-size Root Toe (b,-t) (b,-t) Section b, x b, t r 5, t A Рап y Z V₁ mm mm mm ka/m mm mm mm mm² mm mm 10 mm mm 10 mm mm 125 x 75 x 12 UA 17.7 12.0 10 UA 14.2 9.5 8 UA 11.8 7.8 8.0 5.0 9.42 5.25 2260 8.0 5.0 12.2 6.89 1810 8.0 5.0 15.0 8.62 1500 43.3 18.4 42.3 17.5 3.20 41.5 16.8 2.68 3.91 83.2 83.8 84.2 59.7 31.8…
Figure 3a shows the loading, shear force diagram andbending moment diagram of a simply-supported beamwith its cross-section shown in Figure 3b. Calculatethe maximum bending stress in tension, the maximumbending stress in compression and the maximumshear stress in the beam.
For the beam shown above with length L = 7 m with the applied uniformly distributed load of w = 16 kN/m, what is the maximum bending stress if the beam has a cross section with the following dimensions: b = 100 mm d = 250 mm tf = 20 mm tw = 15 mm
Two uniformly distributed loads of w = 3200 lb/ft act on the simply supported beam shown in Figure A. The beam spans are a = 9.0 ft and L = 17.5 ft. The beam cross section shown in Figure B has dimensions of b₁ = 15.00 in., d₁ = 7.00 in., b₂ = 9.25 in., and d₂ = 11.50 in. Calculate the maximum tensile and compressive bending stresses produced in segment BC of the beam. W a FIGURE A otensile FIGURE B compressive = d₁ d₂ L b₁ b₂ a psi psi X
Two uniformly distributed loads of w = 4100 lb/ft act on the simply supported beam shown in Figure A. The beam spans are a = 7.6 ft and L = 15.0 ft. The beam cross section shown in Figure B has dimensions of b₁ = 15.50 in., d₁ = 6.75 in., b₂ = 10.50 in., and d2 = 10.00 in. Calculate the maximum tensile and compressive bending stresses produced in segment BC of the beam. A W a FIGURE A FIGURE B Otensile = compressive = d₁ d₂ B i i L b₁ b₂ W a psi psi D X
Two uniformly distributed loads of w = 3600 lb/ftact on the simply supported beam shown in Figure A. The beam spans area = 6.8 ft and Z= 15.0 ft. The beam cross section shown in Figure B has dimensions ofb₁ = 15.00 in., d₁ = 5.00 in., b₂ = 11.50 in., and d₂ = 9.75in. Calculate the maximum tensile and compressive bending stresses produced in segment BC of the beam. W a FIGURE A FIGURE B tensile= compressive = d₁ d₂ B i i L b₁ b₂ W a psi psi X
Civil engineering
Analyze the longitudinal schematic diagram of the metal beam shown, taking into account the support conditions, loads and dimensions presented. This diagram was idealized by taking important data from the real situation in the field. The cross section of the beam is rectangular, with a width of b = 80 mm and a height of h = 320 mm. First, find the Maximum Normal Stresses (Tension and Compression) and the Maximum Shear Stresses, showing where they occur (both longitudinally and transversely). Next, find the Normal Stress and Shear Stress at a point 200 mm above the base of the beam and 0.5 m from the left support. Compare your results to the Ultimate Stress or Yield Stress of a material and comment.