Lab #1 Report due TODAY

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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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 - PowerPoint PPT Presentation

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Page 1: Lab #1 Report due TODAY

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

Page 2: Lab #1 Report due TODAY

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

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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

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Stress and Strain

PP B

P FB

r

(a) Tension-Test Specimen

Figure 1.1 Tension-test Specimen (a) Axially Loaded and (b) Cross-Section at B

(b) Cross-Section at B

A

F

L

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Engineering Stress-Strain Curve

, psi

, in/in

u

f

y

ElasticRegion

PlasticRegion

Yield Region

Figure 1.3 Stress-Strain Diagram, Labeled

Elastic Deformation

Uniform Plastic Deformation

Non-uniform Plastic Deformation

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Actual Experimentation

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0.2% Offset Yield Strength

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Modulus of ResilienceModulus of Toughness

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Necking begins at maxima

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Shape of Necked Region

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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)

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Comparison

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Ductile vs. Brittle Failure

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Fracture Surfaces

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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

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Testing Methods

Displacement Control Open loop, Most Common

Load Control Close Loop Feedback, Expensive

Strain Control Close Loop Feedback, Expensive

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Data Sheet

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Data Sheet (continued)

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Demonstration

Perform the tensile testing experiment on

1018 Cold Rolled Steel

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Data Sheet (continued)

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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 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