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Axially loaded member Axial load and normal stress under equilibrium load, Elastic Deformation.

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Presentation on theme: "Axially loaded member Axial load and normal stress under equilibrium load, Elastic Deformation."— Presentation transcript:

1 Axially loaded member Axial load and normal stress under equilibrium load, Elastic Deformation

2 Saint-Venant’s Principle
Localized deformation occurs at each end, and the deformations decrease as measurements are taken further away from the ends At section c-c, stress reaches almost uniform value as compared to a-a, b-b c-c is sufficiently far enough away from P so that localized deformation “vanishes”, i.e., minimum distance

3 Saint-Venant’s Principle
General rule: min. distance is at least equal to largest dimension of loaded x-section. For the bar, the min. distance is equal to width of bar This behavior discovered by Barré de Saint-Venant in 1855, this the name of the principle Saint-Venant Principle states that localized effects caused by any load acting on the body, will dissipate/smooth out within regions that are sufficiently removed from location of load Thus, no need to study stress distributions at that points near application loads or support reactions

4 Elastic Deformation of an Axially Loaded Member
Deformation can be calculated using SIGN CONVENTION When the member is tension When the member is compression

5 Elastic Deformation of an Axially Loaded Member
Total deformation: The Above Figure:

6 Elastic Deformation of an Axially Loaded Member
1) Internal Forces 2) Displacement calculation

7 Example 1 Composite A-36 steel bar shown made from two segments AB and BD. Area AAB = 600 mm2 and ABD = 1200 mm2. Determine the vertical displacement of end A and displacement of B relative to C. A-36 Steel: E = 210 GPa

8 Internal axial load:

9 Displacement of point A
Displacement of point B relative to C

10 Displacement of point A
Displacement of point B relative to C

11 Solve it! The copper shaft is subjected to the axial loads shown. Determine the displacement of end A with respect to end D. The diameter of each segment are dAB = 75 mm, dBC= 50 mm and dCD = 25 mm. Take Ecu = 126 GPa.

12 1) Internal Forces 2) Displacement calculation PAB=30 kN Tension Tension PAB=30 kN P=20 kN PBC=10 kN Compression P=5 kN PCD=-5 kN Total deformation

13 Solve it! The assembly consist of three titanium (Ti-6A1-4V) rods and a rigid bar AC. The cross sectional area for each rod is given in the figure. If a force 30kN is applied to the ring F, determine the angle of tilt of bar AC.

14 1) Equilibrium Equation
FDC 1) Equilibrium Equation F= 30kN FAB 2) Based on FAB and FDC, FDC is predicted to deform more. dDC 3) Angle of tilt dAB Lecture 1

15 Example 2 The assembly shown in the figure consists of an aluminum tube AB having a cross-sectional area of 400 mm2. A steel rod having a diameter of 10 mm is attached to a rigid collar and passes through the tube. If a tensile load of 80 kN is applied to the rod, determine the displacement of the end C of the rod. Take Est = 200 GPa, Eal = 70 GPa.

16 Find the displacement of end C with respect to end B.
Displacement of end B with respect to the fixed end A, Since both displacements are to the right,


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