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Problem 3 σ(ksi) The elastic portion of the tension stress-strain diagram for an aluminum alloy is...
Strength of materials please fast Problem 3.28 Part A The elastic portion of the stress-strain diagram...
Strength of materials please fast
Problem 3.28 Part A The elastic portion of the stress-strain diagram for an aluminum alloy is shown in the figure below Figure 1). The specimen from which it was obtained has an original diameter of 12.7 mm and a gage length of 50.3 mm. Take -0.35 If a load of P 60 kN is applied to the specimen, determine its new diameter Express your answer to four significant figures and include appropriate units |d- 1...
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...
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....
Problem 1 The elastic portion of the stress-strain diagram of the tested material is given below....
Problem 1 The elastic portion of the stress-strain diagram of the tested material is given below. The specimen from which it was obtained had an original diameter of 0.5 in and a gauge length of 2 inches. When the applied load on the specimen is 4573 lb, the diameter is 0.49985 in. Determine the specimen length in inches when the load of 4573 lb is applied and calculate the material's Poisson ratio. Calculate also the rigidity modulus G in ksi....
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....
The stress–strain diagram for a steel alloy having an original diameter of 0.5 in. and a...
The stress–strain diagram for a steel alloy having an original
diameter of 0.5 in. and a gauge length of 2 in. is given in the
figure. If the specimen is loaded until it is stressed to 90 ksi,
determine the approximate amount of elastic recovery and the
increase in the gauge length after it is unloaded. Determine also
approximately the modulus of resilience and the modulus of
toughness for the material.
in. /in.) 0 0 - 0.05 0.10 0.15 0.20...
Draw a schematic stress-strain diagram for steel. Make sure you mark all the important points and regions on it
1. Draw a schematic stress-strain diagram for steel. Make sure you mark all the important points and regions on it. Provide a one-two sentence explanation for each point and region along the diagram. 2. A cylindrical specimen of a nickel alloy having an elastic modulus of 207 GPa (30 x 10* psi) and an original diameter of 10.2 mm (0.40 In.) will experience only elastic deformation when a tensile load of 8900 N (2000 Ibe) is applied. Compute the maximum length...
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...
The stress-strain diagram of an aluminum alloy (initial length=0.06m) is given below. The loading/unloading sequence to...
The stress-strain diagram of an aluminum alloy (initial length=0.06m) is given below. The loading/unloading sequence to the specimen is as follows: A) Load to 600 MPa in tension B) Unload to 0 MPa The expected strain AFTER unloading is: (MPa 600 400 0.0025 0.03 Zero negative Larger than zero but smaller than 0.03 0.0025 0 0.03
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...
Strength of materials please fast
Problem 3.28 Part A The elastic portion of the stress-strain diagram for an aluminum alloy is shown in the figure below Figure 1). The specimen from which it was obtained has an original diameter of 12.7 mm and a gage length of 50.3 mm. Take -0.35 If a load of P 60 kN is applied to the specimen, determine its new diameter Express your answer to four significant figures and include appropriate units |d- 1...
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...
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....
Problem 1 The elastic portion of the stress-strain diagram of the tested material is given below. The specimen from which it was obtained had an original diameter of 0.5 in and a gauge length of 2 inches. When the applied load on the specimen is 4573 lb, the diameter is 0.49985 in. Determine the specimen length in inches when the load of 4573 lb is applied and calculate the material's Poisson ratio. Calculate also the rigidity modulus G in ksi....
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....
The stress–strain diagram for a steel alloy having an original
diameter of 0.5 in. and a gauge length of 2 in. is given in the
figure. If the specimen is loaded until it is stressed to 90 ksi,
determine the approximate amount of elastic recovery and the
increase in the gauge length after it is unloaded. Determine also
approximately the modulus of resilience and the modulus of
toughness for the material.
in. /in.) 0 0 - 0.05 0.10 0.15 0.20...
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...
The stress-strain diagram of an aluminum alloy (initial length=0.06m) is given below. The loading/unloading sequence to the specimen is as follows: A) Load to 600 MPa in tension B) Unload to 0 MPa The expected strain AFTER unloading is: (MPa 600 400 0.0025 0.03 Zero negative Larger than zero but smaller than 0.03 0.0025 0 0.03
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...
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