Question

A cylindrical specimen of a metal alloy 45.3 mm long and 9.72 mm in diameter is...

A cylindrical specimen of a metal alloy 45.3 mm long and 9.72 mm in diameter is stressed in tension. A true stress of 372 MPa causes the specimen to plastically elongate to a length of 54.2 mm. If it is known that the strain-hardening exponent for this alloy is 0.2, calculate the true stress (in MPa) necessary to plastically elongate a specimen of this same material from a length of 45.3 mm to a length of 57.6 mm.

Engineering   Mechanical-Engineering   
0 0
Add a commentTranscribed image text
Next >

Homework Answers

Answer #1

Hence, True stress in cylinder 2 is 419.67 Mpa.

Please Rate,

Thank you...........

0 0
Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Log In

Sign Up

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
A cylindrical specimen of some metal alloy 8.6 mm in diameter is stressed in tension. A...
A cylindrical specimen of some metal alloy 8.6 mm in diameter is stressed in tension. A force of 9070 N produces an elastic reduction in specimen diameter of 0.0048 mm. Calculate the elastic modulus (in GPa) of this material if its Poisson's ratio is 0.33.
A cylindrical specimen of a brass alloy 10.2 mm (0.4016 in.) in diameter and 120.1 mm...
A cylindrical specimen of a brass alloy 10.2 mm (0.4016 in.) in diameter and 120.1 mm (4.728 in.) long is pulled in tension with a force of 12300 N (2765 lbf); the force is subsequently released. The tensile stress-strain behavior for this alloy is shown in the Animated Figure 6.12. Compute the final length of the specimen at this time.
Problem. A cylindrical specimen of a hypothetical metal having a diameter of 7.671 mm and a...
Problem. A cylindrical specimen of a hypothetical metal having a diameter of 7.671 mm and a gauge length of 251.905 mm is pulled in tension. Use the load–elongation characteristics shown in the following table to complete parts (a) through (f). (a) Plot the data as stress (MPa) versus strain (b) Compute the modulus of elasticity in GPa (c) Determine the yield strength at a strain offset of 0.002 (d) Determine the tensile strength of this alloy (e) What is the...
A cylindrical specimen of a brass alloy 10.2 mm (0.4016 in.) in diameter and 120.1 mm...
A cylindrical specimen of a brass alloy 10.2 mm (0.4016 in.) in diameter and 120.1 mm (4.728 in.) long is pulled in tension with a force of 12300 N (2765 lbf); the force is subsequently released. Compute the final length of the specimen at this time. answer in mm.
A cylindrical specimen of a hypothetical metal alloy is stressed in compression. If its original and...
A cylindrical specimen of a hypothetical metal alloy is stressed in compression. If its original and final diameters are 22.623 and 22.651 mm, respectively, and its final length is 79.4 mm, calculate its original length if the deformation is totally elastic. The elastic and shear moduli for this alloy are 104 GPa and 38.3 GPa, respectively.
A tensile test is done on a tensile specimen with a gauge diameter of 8 mm...
A tensile test is done on a tensile specimen with a gauge diameter of 8 mm and gauge length of 45 mm was tested at a temperature above the recrystallization temperature. The test was done at a constant speed of 8 mm/min, strength constant C = 210MPa and strain rate sensitivity exponent m = 0.22. As the gauge length extends to 80 mm then find: The gauge diameter (mm). Tensile force (N). Average flow stress (MPa).
A cylindrical specimen of stainless steel having diameter of 12.8 mm and a guage length of...
A cylindrical specimen of stainless steel having diameter of 12.8 mm and a guage length of 50.88 mm(2.000in.) is pulled in tension. Use the load-elongation characterisitcs shown in the following table. Plot the data as engineering stress vs. engineering strain. Then compute the modulus of elasticity, yeild strength at a strain offset of 0.002, determine the tensile strength of this alloy, approximate ductility in percent elongation and the modulus of resilience. N mm 0 50.8 12700 50.825 25400 50.851 38100...
A normal mild steel specimen having 50 mm 2 cross section area and 10 cm long...
A normal mild steel specimen having 50 mm 2 cross section area and 10 cm long gauge length was tested. 1. Draw the stress- strain diagram 2. calculate the final length of the bar compare when the specimen unloaded from 400 MPa? 3. calculate the elastic and plastic deformation when the specimen unloaded from 400 MPa Proportionality limit Ultimate Load Failure Load Stress (MPa) 320////// 500 /////////400 Strain 0.0018 //// 0.06///////// 0.12
A crack, 1 mm long on the surface, is discovered in a 6061-T651 Al alloy cylindrical...
A crack, 1 mm long on the surface, is discovered in a 6061-T651 Al alloy cylindrical support beam using the eddy current technique. The beam’s diameter is 10 cm. The beam is situated in a aircraft such that it is under a uniform normal stress that is fluctuating. The maximum stress on the beam is 300 MPa. What shape would you assume the crack has? What length would would the crack need to grow to along the surface by fatigue...
Computer electrical conductivity of a Cylindrical silicone specimen 10 mm in diameter and 60 mm in...
Computer electrical conductivity of a Cylindrical silicone specimen 10 mm in diameter and 60 mm in length in which a current of .25 A’s passes in an axial direction. A voltage of 24 V is measured across to probes that are separated by 45 mm. Compute the resistance over the entire 60 mm of the specimen. If the SI specimen has a carrier concentration of 1.5×10^10 m^-3, what is the electron mobility?
ADVERTISEMENT
Need Online Homework Help?

Get Answers For Free
Most questions answered within 1 hours.

Ask a Question
ADVERTISEMENT