Concept explainers
A fatigue test is made with a mean stress of 17,500 psi (120 MPa) and a stress amplitude of 24,000 psi (165 MPa). Calculate (a) the maximum and minimum stresses, (b) the stress ratio, and (c) the stress range.
(a)
The minimum and maximum stress.
Answer to Problem 30AAP
The maximum stress is
Explanation of Solution
Write the expression to calculate stress amplitude.
Here, the stress amplitude is
Write the expression to calculate mean stress.
Here, the mean stress is
Conclusion:
Substitute
Substitute
Substitute
Substitute
Thus, the maximum stress is
(b)
The stress ratio.
Answer to Problem 30AAP
The stress ratio is
Explanation of Solution
Write the expression to calculate stress ratio.
Here, the stress ratio is
Conclusion:
Substitute
Thus, the stress ratio is
(c)
The stress range.
Answer to Problem 30AAP
The stress range is
Explanation of Solution
Write the expression to calculate stress ratio.
Here, the stress range is
Conclusion:
Substitute
Thus, the stress range is
Want to see more full solutions like this?
Chapter 7 Solutions
Foundations of Materials Science and Engineering
Additional Engineering Textbook Solutions
Heat and Mass Transfer: Fundamentals and Applications
Automotive Technology: Principles, Diagnosis, And Service (6th Edition) (halderman Automotive Series)
Vector Mechanics for Engineers: Statics, 11th Edition
Thermodynamics: An Engineering Approach
EBK FUNDAMENTALS OF THERMODYNAMICS, ENH
Engineering Mechanics: Statics
- Draw a typical stress vs strain tensile test curve for the following material and label the axis. A typical brittle material subjected to a tensile stress that has been applied to the material till the sample breaks. 1- label the axis and draw the curve for a brittle material. 2- indicate the maximum strength of the material. 3- show on the portion of the curve where young's modulus can be calculated.arrow_forwardState and explain the theories of failures applicable to Brittle material.arrow_forward-Define the maximum shear stress theory and sketch its failure envelope.-Define the maximum shear strain energy theory and sketch its failure envelopearrow_forward
- During a high cycle fatigue test, a metallic specimen is subjected to cyclic loading with a mean stress of +140 MPa, and a minimum stress of – 70 MPa.find out the R-ratio for this cyclic loading.arrow_forwardThe sketch below shows a material with a crack of length 2a, and a nominal stress of s0. You are informed that the stress at the tip is 8 s0. The fracture stress of the material is 12 s0. 1) what is the radius of curvature of the crack tip? 2) if the radius of curvature is reduced further by a factor of 2, will the local tip stress now exceed the fracture stress?arrow_forwardDraw a typical stress vs strain tensile test curve for the following materials (two seperate graphs) and label the axis. A ductile metallic test specimen that is stretched to failure displaying a characteristic yield point and show the following parts on the curve. 1- Yield point 2- Ultimate Tensile Strength 3- Breaking point 4- Elastic Region 5- Plastic Region 6- Necking regionarrow_forward
- For the given fluctuating fatigue koad, the values of stress amplitude and stress ratio are.arrow_forwardTensile and fully reversed loading fatigue tests were conducted for a certain steel alloy and revealed the tensile strength and endurance limit to be 1200 and 550 MPa, respectively. If a rod of this material supply were subjected to a static stress of 600 MPa and oscillating stresses whose total range was 700 MPa, would you expect the rod to fail by fatigue processes? Hint: You may want to plot a diagram to aid in presenting your answer.arrow_forwardFor the given fluctuating fatigue load,the values of stress amplitude and stress ratio are respectively???arrow_forward
- C and D c) Determine the fatigue lifetimes at stress amplitudes of 230 MPa and 175 MPa?d) Estimate the maximum lifetime of continuous driving that are allowable for the following 250 MPa and 150 MPa stress levels.arrow_forward7. By referring to a sketch showing a stress concentration, describe the phenomenon of crack initiation in high cycle fatigue and comment on the proportion of fatigue life that is used in initiating a crack under these conditions. 8. By considering a notched metal bar as an example, explain (with the aid of diagrams), how you would reduce the probability of fatigue failure by applying self-stresses. 9. Describe, with sketched examples, how the stress-raising effect of circular and elliptical holes can be considered qualitatively as being analogous to liquid flow. 10. By considering a circular hole in a thin elastic sheet, explain (with the aid of any diagrams as appropriate) how a stress concentration can magnify stress. 11. Explain the principles of designing alloys for oxidation resistance.12. Describe and explain (with the aid of a sketch) how crack propagation is enhanced through stress corrosion cracking Answer All partsarrow_forward8.a) Calculate the theoretical fracture strength of a brittle material wherein fracture occurs by propagation of an elliptically shaped 0.25 mm surface crack with a 1.2 × 10-3 mm tip radius under an applied 1200 MPa stress. b) If the specific surface energy for a material is 0.30 J/m2 and its elastic modulus is 69 GPa, calculate the minimum stress required for propagation of a surface crack 0.05 mm in length. Based on this calculation, estimate the materials fracture toughness.arrow_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