
Concept explainers
The material for a rod of cross-sectional area 2.70 in.2 and length 75.0 in. must be selected such that under an axial load of 120.000.0 lb. it will not yield and the elongation in the bar will remain below 0.105 in. (a) Provide a list of at least three different metals that would satisfy these conditions. (b) Narrow the list down if cost is an issue, (c) Narrow the list down if corrosion is an issue. Use Appendix I for properties and cost of common alloys only.
a)

The list of three different metals which satisfy the given condition.
Explanation of Solution
Write the expression for the stress acting in the rod.
Here, applied force is
Write the expression for the engineering strain as given as follows:
Here, change in length is
Write the expression for the Hook’s law as given as follows:
Here, stress is
Conclusion:
Substitute 120,000 lb for
Substitute 0.105 in for
The given rod is loaded with in the elastic region so hook’s law can be applied for obtaining the stress and strain values.
Substitute
The material that needs to satisfy the given specification should possess at least 200 GPa as Young’s modulus.
Refer the Appendix I, “5. Room temperature modulus of elasticity” obtain the following metals whose Young’s modulus values are equal to or more than 200 GPa.
- 1. Low alloy steels (Alloy 1006 cold drawn)
- 2. Stainless steels (Alloy 405 cold rolled annealed)
- 3. Miscellaneous alloys (Hayness 25 cold rolled and annealed)
b)

Choose the material based on the cost of the material.
Explanation of Solution
Refer the Appendix I “16. Cost and relative cost of some selected materials” obtain the cost of metals that are chosen in part (a) whose young’s modulus values are more than 218.66 GPa .
- 1. Low alloy steels (Alloy 1006 cold drawn) – 2.91 US $/lb
- 2. Stainless steels (Alloy 405 cold rolled annealed) – 394.79 US $/lb
- 3. Miscellaneous alloys (Hayness 25 cold rolled and annealed) – 40US $/lb
If cost is an issue, the best choice is Low alloy steels (Alloy 1006 cold drawn).
c)

Choose the material based on the cost of the corrosion.
Explanation of Solution
Refer part (a).
The materials are,
- 1. Low alloy steels (Alloy 1006 cold drawn)
- 2. Stainless steels (Alloy 405 cold rolled annealed)
- 3. Miscellaneous alloys (Hayness 25 cold rolled and annealed)
Residual stresses are induced when the material is cold worked. This residual stresses can cause corrosion, with proper annealing heat treatment residual stresses can be removed. Hence, comparing the stainless steels with miscellaneous alloys, the stainless steels will be the good choice and prevents the corrosion. Stainless steel alloys are readily available in the market.
Want to see more full solutions like this?
Chapter 6 Solutions
Foundations of Materials Science and Engineering
Additional Engineering Textbook Solutions
Vector Mechanics For Engineers
Thermodynamics: An Engineering Approach
Electric Circuits. (11th Edition)
BASIC BIOMECHANICS
Automotive Technology: Principles, Diagnosis, And Service (6th Edition) (halderman Automotive Series)
Java: An Introduction to Problem Solving and Programming (8th Edition)
- (Read Image)arrow_forwardM16x2 grade 8.8 bolts No. 25 C1- Q.2. The figure is a cross section of a grade 25 cast-iron pressure vessel. A total of N, M16x2.0 grade 8.8 bolts are to be used to resist a separating force of 160 kN. (a) Determine ks, km, and C. (b) Find the number of bolts required for a load factor of 2 where the bolts may be reused when the joint 19 mm is taken apart. (c) with the number of bolts obtained in (b), determine the realized load factor for overload, the yielding factor of safety, and the separation factor of safety. 19 mmarrow_forwardProblem4. The thin uniform disk of mass m = 1-kg and radius R = 0.1m spins about the bent shaft OG with the angular speed w2 = 20 rad/s. At the same time, the shaft rotates about the z-axis with the angular speed 001 = 10 rad/s. The angle between the bent portion of the shaft and the z-axis is ẞ = 35°. The mass of the shaft is negligible compared to the mass of the disk. a. Find the angular momentum of the disk with respect to point G, based on the axis orientation as shown. Include an MVD in your solution. b. Find the angular momentum of the disk with respect to point O, based on the axis orientation as shown. (Note: O is NOT the center of fixed-point rotation.) c. Find the kinetic energy of the assembly. z R R 002 2R x Answer: H = -0.046ĵ-0.040 kg-m²/sec Ho=-0.146-0.015 kg-m²/sec T 0.518 N-m =arrow_forward
- Problem 3. The assembly shown consists of a solid sphere of mass m and the uniform slender rod of the same mass, both of which are welded to the shaft. The assembly is rotating with angular velocity w at a particular moment. Find the angular momentum with respect to point O, in terms of the axes shown. Answer: Ñ。 = ½mc²wcosßsinßĵ + (}{mr²w + 2mb²w + ½ mc²wcos²ß) k 3 m r b 2 C لا marrow_forwardOnly question 2arrow_forwardOnly question 1arrow_forward
- Only question 3arrow_forwardI have Euler parameters that describe the orientation of N relative to Q, e = -0.7071*n3, e4 = 0.7071. I have Euler parameters that describe the orientation of U relative to N, e = -1/sqrt(3)*n1, e4 = sqrt(2/3). After using euler parameter rule of successive rotations, I get euler parameters that describe the orientation of U relative to Q, e = -0.4082*n1 - 0.4082*n2 - 0.5774*n3. I need euler parameters that describe the orientation of U relative to Q in vector basis of q instead of n. How do I get that?arrow_forwardDescribe at least 4 processes in engineering where control charts are (or should be) appliedarrow_forward
- Describe at least two (2) processes where control charts are (or should be) applied.arrow_forwardProblem 3: A cube-shaped spacecraft is in a circular Earth orbit. Let N (n,) be inertial and the spacecraft is denoted S (ŝ₁). The spacecraft is described such that ¯½º = J ŝ₁ŝ₁ + J ŝ₂§₂ + J §¸Ŝ3 Location of the spacecraft in the orbit is determined by the orbit-fixed unit vectors ê, that are oriented by the angle (Qt), where is a constant angular rate. 52 €3 3> 2t 55 Λ Из At the instant when Qt = 90°, the spacecraft S is oriented relative to the orbit such that 8₁ = 0° Space-three 1-2-3 angles 0₂ = 60° and ES = $₂ rad/s 0₁ = 135° (a) At this instant, determine the direction cosine matrix that describes the orientation of the spacecraft with respect to the inertial frame N.arrow_forwardThis problem illustrates that the factor of safety for a machine element depends on the particular point selected for analysis. Here you are to compute factors of safety, based upon the distortion-energy theory, for stress elements at A and B of the member shown in the figure. This bar is made of AISI 1006 cold-drawn steel and is loaded by the forces F = 1.100 kN, P = 8.00 kN, and T = 50.00 N-m. Given: Sy = 280 MPa. B -100 mm- 15-mm D. a) Determine the value of the axial stress at point B. b) Determine the value of the shear stress at point B. c) Determine the value of the Von Mises stress at point B. P Farrow_forward
- Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University PressMechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSONThermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
- Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEYMechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage LearningEngineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY





