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Lab #1 Report due TODAY Individual Data Processing and Individual Write Up Lab #1 Report is due TODAY by midnight Answer Multiple Choice Questions ONLINE.

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Presentation on theme: "Lab #1 Report due TODAY Individual Data Processing and Individual Write Up Lab #1 Report is due TODAY by midnight Answer Multiple Choice Questions ONLINE."— Presentation transcript:

1 Lab #1 Report due TODAY Individual Data Processing and Individual Write Up Lab #1 Report is due TODAY by midnight Answer Multiple Choice Questions ONLINE TODAY by midnight Answer Student Survey ONLINE TODAY by midnight Submit the Lab Report #1 in the drawer labeled “MECE204 - Strength Lab” under Mech. Engg. Mail Folders

2 Tensile Testing: Objectives
Learn elastic and plastic behavior of metallic materials in monotonic tension Learn the use of Tinius Olsen 120 kips UTS and clip-on extensometer Conduct tensile testing experiment on 1018 steel and 2024 aluminum alloy Determine quantitatively elastic and tensile mechanical properties Determine qualitatively the material’s failure mode Become familiar with ASTM E-8 Standard Submit a professional lab report with abstract, data, graphs, and discussion Answer multiple-choice questions and student survey ONLINE using MyCourses

3 Tensile Properties Quantitative determination of
Elastic Modulus, E Proportional Limit, PL 0.2% Offset Yield Strength, Y Tensile Strength, TS % Elongation to Failure, %f Modulus of Toughness, Atotal Qualitative study of Failure

4 Stress and Strain (b) Cross-Section at B (a) Tension-Test Specimen
F B r (b) Cross-Section at B Figure 1.1 Tension-test Specimen (a) Axially Loaded and (b) Cross-Section at B

5 Engineering Stress-Strain Curve
Non-uniform Plastic Deformation Uniform Plastic Deformation Elastic Deformation s , psi e , in/in su sf sy Elastic Region Plastic Yield Region Figure 1.3 Stress-Strain Diagram, Labeled

6 Actual Experimentation

7 0.2% Offset Yield Strength

8 Modulus of Resilience Modulus of Toughness

9 Necking begins at maxima

10 Shape of Necked Region

11 Engineering vs. True Stress-Strain
Engineering Stress = e = P / A0 True Stress = t = P / Ai Engineering Strain = e =  / L0 = (Li – L0) / L0 implies Li = L0 * (1 + e) Assume volume is constant until necking: A0*L0 = Ai*Li  Ai = A0/(1+e) True Stress = t = P / Ai = P (1 + e) / A0 = e (1 + e) True Strain = t =  (dL)/L = Ln(Li / L0) = Ln (1 + e)

12 Comparison

13 Ductile vs. Brittle Failure

14 Fracture Surfaces

15 Testing Equipment Universal Testing Machine (UTM)
Tension, Compression and Flexure Monotonic Static Tension Test Single direction, Load increased slowly Crosshead Motion Motor-driven Screw Hydraulically-driven Crosshead ASTM Standards: E8

16 Testing Methods Displacement Control Load Control Strain Control
Open loop, Most Common Load Control Close Loop Feedback, Expensive Strain Control

17 Data Sheet

18 Data Sheet (continued)

19 Demonstration Perform the tensile testing experiment on
1018 Cold Rolled Steel

20 Data Sheet (continued)

21 Lab #1 Report due TODAY Individual Data Processing and Individual Write Up Lab #1 Report is due TODAY by midnight Answer Multiple Choice Questions ONLINE TODAY by midnight Answer Student Survey ONLINE TODAY by midnight Submit the Lab Report #1 in the drawer labeled “MECE204 - Strength Lab” under Mech. Engg. Mail Folders


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