Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
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What is the hardening exponential n and deformation rate sensitivity exponential m ? Comment similar or different aspects, their numerical values should be big or small and changes with temperature
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- Example: Consider a metal whose strain hardening behavior follows: 25,000 0.25 psi. If an annealed bar of this metal is pulled in a tension test from a starting dia. of 12.7mm to a dia. of 11.5mm (uniform elongation, no friction, no distortion), what is the work per unit volume required? If the bar is reduced by extruding and the deformation efficiency is 70%, what is the extrusion pressure?arrow_forward10 - Prob 7. Steady - state creep data taken for stainless steel at a stress level of 70 MPa (10,000 psi) are given as follows: (8 marks) If it is known that the value of the stress exponent n for this alloy is 7.0, compute the steady - state creep rate at 1250 K and a stress level of 50 Mpa. é, (s-1) T (K) 1.0 X 10-5 2.5 X 10-3 977 1089arrow_forward8.15 List four major differences between defor- mation by twinning and deformation by slip relative to mechanism. conditions of occur- rence, and final result. 8.17 Briefly explain why HCP metals are typically more brittle than FCC and BCC metals. 8.5 a) Define a slip system. ) Do all Do all metals have the same slip system? Why or why not? " 8.42 Briefly explain how each of the following influences the tensile modulus of a semicrys- talline polymer and why: (a) molecular weight; (b) degree of crystallinity; (c) deformation by drawing: (d) annealing of an undeformed material; (e) annealing of a drawn material.arrow_forward
- An S-N plot from fatigue testing of a steel is provided below. Use the plot to determine the following values for this steel. 1. Fatigue limit: 2. Fatigue lifetime at a stress amplitude of: 415 MPa: 275 MPa: 3. Fatigue strength at: 5x104 cycles: 5x105 cycles 500 400 300 200 100 0 1.E+04 Stress Amplitude (MPa) 1.E+05 1.E+06 Cycles to Failure 1.E+07 1.E+08arrow_forwardStuck need help! Problem is attached. please view attachment before answering. Really struggling with this concept. Please show all work so I can better understand ! Thank you so much.arrow_forwardSuppose that the material in Q4 is fabricated in 25 mm (1 in) thick plate, estimate the largest valid K1c that can be measured on such a specimen.arrow_forward
- A flat-rolling operation of 250 mm wide alloy stee Calculate roll torquearrow_forward1. Briefly explain the difference between hardness and hardenability.arrow_forwardb) A 1-cm-thick copper plate is cold-reduced to 0.50 cm and later further reduced to 0.16 cm. Determine I. The total percent cold work and Il- Predict the properties of the metal at the calculated cold work? 0.16 cm I cm 0.5 cm, Figure-2arrow_forward
- 7-5arrow_forward70% + | 8 0 4. An application requires ultimate tensile strength and yield strength of a steel at 110 ksi and 91 ksi, respectively. A data table is attached in the back of the test. Answer the following 4 questions: 4.1. Can SAE 1040 steel be selected for this application? 4.2. If "no" is the answer in Part I, the following Part II, III, and IV can be ignored. If "yes" is the answer in Part I, which condition of SAE 1040 should be selected? 4.3. Why is that steel with the condition in part II selected? 4.4. Is the selected steel brittle or ductile? and Why? Page 4 of 6arrow_forwardi need the answer quicklyarrow_forward
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