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MATE 1104 TENSILE TEST LAB HANDOUT In your lab write-up please include the following: 1. Cover Page 2. Purpose 3. Calculations: Calculate the following

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MATE 1104 TENSILE TEST LAB HANDOUT In your lab write-up please include the following: 1. Cover Page 2. Purpose 3. Calculations: Calculate the following for each graph: Area of test coupon Ultimate Tensile Strength 0.2% Offset Yield Strength % Elongation % Reduction of Area Modulus of Elasticity (1045 steel only) 4. Plot the Stress-Strain curve for the 44W sample by hand You are given the Load-Strain curve for the 44W sample You must convert the Load-Strain curve to Stress-Strain Show a sample calculation for determining the stress value at a particular load Create a data table to indicate the loads and the corresponding stress values and its strain value 5. Label each graph (44W and 1045 steel) with the following: Ultimate tensile strength (UTS) Yield Point (44W only) Proportional Limit (1045 material only) 0.2% offset yield strength Elastic Region Plastic Region Title of Graph 6. Results/Discussion Discuss what the effect of carbon content has on each material. b. Determine what the converted Rockwell hardness would be for each material (refer C. to page. 10 in course pack 2589) What can be said regarding the mechanical properties (ductility, strength & hardness) of each material? Test #1: 44W Steel Original Diameter: 0.625 5) Original Area:_ Original Length: 2.00' Maximum Load: Final Diameter: 0.356 Final Area: Final Length: 2.837 Yield Load: Calculate: Load (lbs) Area of test coupon Ultimate Tensile Strength (UTS) 0.2% Yield Strength (YS) % Elongation % Reduction of Area Test #2: 1045 Steel Original Diameter: Original Area:_ Strain (in/in) Stress (lbs/in) 0.625 $9 Final Diameter: 0.496 Original Length: 2.000 Maximum Load: Calculate: Final Area: " Final Length: 2.303 Yield Load: Area of test coupon Ultimate Tensile Strength (UTS) 0.2% Yield Strength (YS) % Elongation % Reduction of Area Modulus of Elasticity 0 Force (lbf) 30,000 27,000 24,000 21,000 18,000 15,000 12,000 9,000 6,000 3,000 Flow * Acad is Same J. type TR < Ene Ident Fy box A Method Name: Output Name: Material: Operator: Diameter: NAIT Materials Eng. Tech. UTM #1 Tensile Imperial - Student / Load vs Si Tensile Imperial - Student / MP 44W MN 0.625 in Ultimate Force: 21900 lbf Break Force: 14300 lbf 0.001 0.002 0.003 0.004 0.005 0.006 0.007 0.008 0.009 0.010 Strain (in/in) Tensile Imperial - Student / Load vs Strain (Epsilon Ext)(Original), (rev. 5) 253-339767US - NAIT Output. Tensile Imperial - Stue Hydraulic (602)/1.3: 120000lbf. Printed: 2022-C

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