and a gage length of 5 Is shown in the figure below a) Determine the modulus of resilience b) Determin the modulus of toughness
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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 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....
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 1: A tension test was performed on a steel specimen having an original diameter of 0.50 in. and gage length of 2.00 in. The final diameter is de .38 in. The data is listed in the table. 1) Plot the stress-strain diagram on engineering paper, so you can calculate the area easily; 2) Determine approximately the modulus of elasticity; 3) Find the yield stress by 0.2% offset method; 4) Calculate approximately the modulus of resilience; 5) Determine approximately the...
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...
please be very 100% sure before doing. thank you (1) (25 points) Load-elongation dataset were obtained from a tensile test of high-strength steel as shown in the table. The test specimen had a diameter of 0.505 in. and a gage length of 2.00 in. The Poisson's ratio of high-strength steel is found to be 0.33 At fracture, the elongation between the gage marks was 0.12 in and the minimum diameter was 0.42 in 1) Plot the engineering stress-strain curve using...
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