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The stress–strain diagram for a steel alloy having an original
diameter of 0.5 in. and a...
3-5. The stress-strain diagram for a steel alloy having an original diameter of 12 mm and...
3-5. The stress-strain diagram for a steel alloy having an original diameter of 12 mm and a gauge length of 50 mm is given in the figure. If the specimen is loaded until it is stressed to 500 MPa, determine the approximate amount of elastic recovery and the increase in the gauge length after it is unloaded. O (MPa) 600 - E(mm/mm) 0 0 0.04 0.08 0.12 0.16 0.20 0.24 0.28 0.0005 0.001 0.0015 0.002 0.0025 0.003 0.0035 Prob. 3-5
Question #3: The stress-strain diagram for a steel alloy having an original diameter of 0.45 in....
Question #3: The stress-strain diagram for a steel alloy having an original diameter of 0.45 in. and a gage length of 2.5 in. is given in the Fig. If the specimen is loaded until it is stressed to 75 ksi, determine the modulus of elasticity for the material, amount of elastic recovery, the increase in the gage length, and modulus of resilience (ur) before and after the load application. σ (ksi) 80 70 60 50 40 30 20 10 e...
Problem No. 2 (Figure 2) (ksi) Figure 2. Upper scale Lower scale The stress-strain diagram of...
Problem No. 2 (Figure 2) (ksi) Figure 2. Upper scale Lower scale The stress-strain diagram of a mild-steel specimen is shown in the figure. The specimen has a diameter of 0.50-inch and gage length of 2-inch. Determine the following: (a) yield strength (oy); (b) ultimate strength (out); (c) Young's modulus (E); (d) modulus of resilience; (e) if the specimen is loaded to 105 ksi and then unloaded completely, determine the permanent increase in the gage length € (in/in) 0 0.04...
Problem 3.12 The stress-strain diagram for an aluminum alloy specimen having an original diameter of 0.5...
Problem 3.12 The stress-strain diagram for an aluminum alloy specimen having an original diameter of 0.5 in and a gage length of 2 in is shown in the figure below. (Figure 1) Figure 1 of 1 > o (ksi) 70 60 50 40 30 20 10 0 0.02 0.04 0.06 0.08 0.10 0.12 0.14 0.16 0.18 0.2 € (in./in.) 0 0.0025 0.0050.0075 0.01 0.0125001500175 0.02 0.02550025 VAL nili Determine the modulus of resilience. Express your answer to three significant figures....
Strength of material The stress-strain diagram for an aluminum alloy specimen having an original diameter of...
Strength of material
The stress-strain diagram for an aluminum alloy specimen having an original diameter of 0.5 in. and a gage length of 2 in, is shown in the figure below. σ (ksi) 70 60 50 40 30 20 10 0 e (in./in.) 0 0.02 0.04 0.06 0.08 0.10 0.12 0.14 0.16 0.18 0.2 0 00025 0.0050.0075 0.01 0.0125001500175 0.02 00255 0.025 Tap image to zoom Part A Determine the modulus of resilience. Express your answer to three significant figures....
Q1 (10 points): Consider the two stress-strain curves shown to the right. Based on each of...
Q1 (10 points): Consider the two stress-strain curves shown to the right. Based on each of these stress-strain curves, calculate or identify the following items: (a) • Modulus of elasticity Yield stress Yield strain Ultimate stress Ultimate strain Fracture stress Fracture strain • Ductility ratio Modulus of resilience Modulus of toughness u oo Stress (ksi) Straini 0.0012 0.0031 0.0039 0.0064 0.0079 O Note: If any of the values you need to identify or calculate are not explicitly clear from the...
2) Using the stress-strain curve for a steel alloy shown in the following figure answer the...
2) Using the stress-strain curve for a steel alloy shown in the following figure answer the following questions: 600 500 400 500 400 300 300 200 200 100 100 0.000 0.002 0.006 0.004 Strain 0.00 0,04 0.08 0.12 0.16 0.20 Using the same steel alloy, consider a cylindrical specimen 15 mm in diameter pulled in tension, if a load of 85,000 N is applied: h) Calculate the approximate ductility in percent elongation, (consider the final elongation as the elongation at...
(c) Acylindrical specimen of stainless steel having a diameter of 12.8 mm and a gauge length...
(c) Acylindrical specimen of stainless steel having a diameter of 12.8 mm and a gauge length of 50.800 mm is pulled in tension. The data acquired was used to plot engineering stress versus engineering strain as shown in the following two graphs (please note that fig. b is a blown-up clastic portion of (a)). Use the o-curves to complete parts through (vi) Stress (MP) 0.00 0.02 0.04 0.06 0.08 0.10 Strain Fig (a). - curve of stainless steel Stress (MPa)...
PROBLEM5 A tensile test specimen of stainless steel alloy having a diameter of 0.495 inches and...
PROBLEM5 A tensile test specimen of stainless steel alloy having a diameter of 0.495 inches and a gage length of 2.00 in was tested to fracture. Stress and strain data obtained during the test are shown below. Determine a. The modulus of elasticity b. The proportional limit c. the ultimate strength d, the yield strength (with a 0.20% offset) 160 Upper scale 120 Lower scale 40 0.0 0.020 0.040 0.060 0.080 0.100 0.120 L-Le 0.0 0.002 0.004 0.006 0.008 0.010...
Problem 3 σ(ksi) The elastic portion of the tension stress-strain diagram for an aluminum alloy is...
Problem 3 σ(ksi) The elastic portion of the tension stress-strain diagram for an aluminum alloy is shown in the figure. The specimen used for the test has a gage length of 2 in. and a diameter of 0.5 in. If the applied load is 10 kip, determine the new diameter of the specimen. The shear modulus is G-3.8(10') ksi. 60
3-5. The stress-strain diagram for a steel alloy having an original diameter of 12 mm and a gauge length of 50 mm is given in the figure. If the specimen is loaded until it is stressed to 500 MPa, determine the approximate amount of elastic recovery and the increase in the gauge length after it is unloaded. O (MPa) 600 - E(mm/mm) 0 0 0.04 0.08 0.12 0.16 0.20 0.24 0.28 0.0005 0.001 0.0015 0.002 0.0025 0.003 0.0035 Prob. 3-5
Question #3: The stress-strain diagram for a steel alloy having an original diameter of 0.45 in. and a gage length of 2.5 in. is given in the Fig. If the specimen is loaded until it is stressed to 75 ksi, determine the modulus of elasticity for the material, amount of elastic recovery, the increase in the gage length, and modulus of resilience (ur) before and after the load application. σ (ksi) 80 70 60 50 40 30 20 10 e...
Problem No. 2 (Figure 2) (ksi) Figure 2. Upper scale Lower scale The stress-strain diagram of a mild-steel specimen is shown in the figure. The specimen has a diameter of 0.50-inch and gage length of 2-inch. Determine the following: (a) yield strength (oy); (b) ultimate strength (out); (c) Young's modulus (E); (d) modulus of resilience; (e) if the specimen is loaded to 105 ksi and then unloaded completely, determine the permanent increase in the gage length € (in/in) 0 0.04...
Problem 3.12 The stress-strain diagram for an aluminum alloy specimen having an original diameter of 0.5 in and a gage length of 2 in is shown in the figure below. (Figure 1) Figure 1 of 1 > o (ksi) 70 60 50 40 30 20 10 0 0.02 0.04 0.06 0.08 0.10 0.12 0.14 0.16 0.18 0.2 € (in./in.) 0 0.0025 0.0050.0075 0.01 0.0125001500175 0.02 0.02550025 VAL nili Determine the modulus of resilience. Express your answer to three significant figures....
Strength of material
The stress-strain diagram for an aluminum alloy specimen having an original diameter of 0.5 in. and a gage length of 2 in, is shown in the figure below. σ (ksi) 70 60 50 40 30 20 10 0 e (in./in.) 0 0.02 0.04 0.06 0.08 0.10 0.12 0.14 0.16 0.18 0.2 0 00025 0.0050.0075 0.01 0.0125001500175 0.02 00255 0.025 Tap image to zoom Part A Determine the modulus of resilience. Express your answer to three significant figures....
Q1 (10 points): Consider the two stress-strain curves shown to the right. Based on each of these stress-strain curves, calculate or identify the following items: (a) • Modulus of elasticity Yield stress Yield strain Ultimate stress Ultimate strain Fracture stress Fracture strain • Ductility ratio Modulus of resilience Modulus of toughness u oo Stress (ksi) Straini 0.0012 0.0031 0.0039 0.0064 0.0079 O Note: If any of the values you need to identify or calculate are not explicitly clear from the...
2) Using the stress-strain curve for a steel alloy shown in the following figure answer the following questions: 600 500 400 500 400 300 300 200 200 100 100 0.000 0.002 0.006 0.004 Strain 0.00 0,04 0.08 0.12 0.16 0.20 Using the same steel alloy, consider a cylindrical specimen 15 mm in diameter pulled in tension, if a load of 85,000 N is applied: h) Calculate the approximate ductility in percent elongation, (consider the final elongation as the elongation at...
(c) Acylindrical specimen of stainless steel having a diameter of 12.8 mm and a gauge length of 50.800 mm is pulled in tension. The data acquired was used to plot engineering stress versus engineering strain as shown in the following two graphs (please note that fig. b is a blown-up clastic portion of (a)). Use the o-curves to complete parts through (vi) Stress (MP) 0.00 0.02 0.04 0.06 0.08 0.10 Strain Fig (a). - curve of stainless steel Stress (MPa)...
PROBLEM5 A tensile test specimen of stainless steel alloy having a diameter of 0.495 inches and a gage length of 2.00 in was tested to fracture. Stress and strain data obtained during the test are shown below. Determine a. The modulus of elasticity b. The proportional limit c. the ultimate strength d, the yield strength (with a 0.20% offset) 160 Upper scale 120 Lower scale 40 0.0 0.020 0.040 0.060 0.080 0.100 0.120 L-Le 0.0 0.002 0.004 0.006 0.008 0.010...
Problem 3 σ(ksi) The elastic portion of the tension stress-strain diagram for an aluminum alloy is shown in the figure. The specimen used for the test has a gage length of 2 in. and a diameter of 0.5 in. If the applied load is 10 kip, determine the new diameter of the specimen. The shear modulus is G-3.8(10') ksi. 60
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