Concept explainers
One of the important considerations when selecting a material for an application is to determine the highest and lowest operating temperature along with the companion properties that must be present at each extreme. The ductile�to�brittle transition temperature, discussed in Section 2.4, has been an important factor in a number of failures. An article that summarized the features of 56 catastrophic brittle fractures that made headline news between 1888 and 1956 noted that low temperatures were present in nearly every case. The water temperature at the time of the sinking of the Titanic was above the freezing point for salt water, but below the transition point for the steel and rivets used in construction of the hull of the ship.
- Which of the common engineering materials exhibits a ductile�to�brittle transition?
- For plain carbon and low�alloy steels, what is a typical value (or range of values) for the transition temperature?
- What type of material would you recommend for construction of a small vessel to transport liquid nitrogen within a building or laboratory?
- Figure 2.35 summarizes the results of impact testing performed on hull plate from the RMS Titanic and similar material produced for modern steel�hulled ships. Why should there be a difference between specimens cut longitudinally (along the rolling direction) and transversely (across the rolling direction)? What advances in steel making have led to the significant improvement in low�temperature impact properties?
Want to see the full answer?
Check out a sample textbook solutionChapter 2 Solutions
Degarmo's Materials And Processes In Manufacturing
- Estimate the theoretical fracture strength (in MPa) of a brittle material if it is known that fracture occurs by the propagation of an elliptically shaped surface crack of length 0.25 mm that has a tip radius of curvature of 0.004 mm when a stress of 1060 MPa is applied.arrow_forwarddraft is 10.nm Q2: The following stress and strain values were measured in the plastic region during a tensile test carried out on a new experimental metal: (1) true stress = 43.608 lb/in2 and true strain = 0.27. (2) true stress = 52.048 lb/in2 and true strain = 0.85. Based on these data points, determine the (strength coefficient and strain- hardening exponent. Find the engineering stress and strain at the second nointarrow_forwardSketch Figure 1.3, curve b (a ductile metal). Label it with the following terms, indicating from which location on the curve each quantity can be identified or extracted: elastic region, plastic region, proportional limit, tensile strength, onset of necking, fracture stress.arrow_forward
- The 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_forwardDo the irregularities vary from specimen to specimen in tensile fracture?arrow_forwardA structural component is fabricated from an alloy that has a plane strain fracture toughness of 45 MPa√√m. It has been determined that this component fails at a stress of 300 MPa when the maximum length of a surface crack is 0.95 mm. What is the maximum allowable surface crack length (in mm) without fracture for this same component exposed to a stress of 300 MPa and made from another alloy with a plane-strain fracture toughness of 57.5 MPa√m?arrow_forward
- A structural component in the shape of a flat plate 24.2 mm thick is to be fabricated from a metal alloy for which the yield strength and plane strain fracture toughness values are 537 MPa and 28.2 MPa-m¹/2, respectively. For this particular geometry, the value of Y is 1.9. Assuming a design stress of 0.4 times the yield strength, calculate the critical length of a surface flaw. i mmarrow_forward3. Linear elastic fracture mechanics (LEFM) predicts there will be an infinite stress at the tip of a crack. Why is this not the case? What happens microstructurally in metals, polymers and ceramics that prevents this?arrow_forward6. A ceramic part for a jet engine has a yield strength of 648 MPa and a plane strain fracture toughness of 8.49 MPam 4. To be sure that the part does not fail, we plan to ensure that the maximum applied stress is only one-third of the yield strength. We use a nondestructive test that will detect any internal flaws greater than 0.27 mm long. Assuming that the Y constant is 1.4, does our nondestructive test have the required sensitivity? Explain.arrow_forward
- According to Griffith's theory for brittle fracture, the stress required to propagate a crack is: (This question has more than one correct answer) 0.5 a. Proportional to a' where 2a is the crack length b. More than the ideal fracture stress -0.5 c. Proportional to a d. Less than the ideal fracture stress e. Proportional to the surface energy y0.5 f. Proportional to the surface energy yarrow_forwardEngineering Metallurgyarrow_forwardDiscussion : • Difficulties in testing brittle materials. • Advantages of stress - strain diagram. • Sources of error you expect in the experiment. • Define the term strain hardening and explain in which stage in the stress- strain diagram it occurs, what are its reasons, and its effects on material properties? • Compare between the brittle and ductile fracture. fr in tearrow_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