(6) Plain Strain
Explanation: Plain Strain is the condition in which strain in one direction is zero.
(7) Higher, more likely
Explanation: Sharper the fillet radius means more stress concentration which leads to more likely failure of object.
(8) False
Explanation: FCC doesn't experience ductile to brittle transition.
(9) Fatigue limit
Explanation: Fatigue limit is the stress level below which an infinite number of loading cycles can be applied to a material without causing fatigue failure.
(10) Secondary region
Explanation: In secondary region strain rate is constant.
Question 6 1 pts When a material doesn't change its strain perpendicular to the loading condition,...
A. If a material is tested in the linear part of the engineering stress-strain curve, what is expected behavior? B. Define the two trigonometric parameters in the definition of critical resolved shear stress C. How can hardness be used in determining the tensile strength? D. If an alloy is produced with a fine grain size, will it have higher or lower strength an opposed to igcoarse grained counterpart? E. How can solid solutions enhance strength? ! F. What is the...
1. A large plate is fabricated from a steel alloy that has a plane strain fracture toughness of 82.4 MPavm. If the plate is exposed to a tensile stress of 345 MPa during service use, determine the minimum length of a surface crack that will lead to fracture. Assume a value of 1.0 for Y. Maximum stress at tip of elliptically shaped crack Pt 2Ery, 1/2 critical stress required for crack propagation in a brittle material πα KIe YoeVra Fracture...
6) Plastic deformation in a ductile machine ch question 10 points element causing separation into multiple pieces a. Ductile rupture b. Buckling c. Brittle fracture d. Fatigue 1) Plastic deformation amplified by high temperature operation over time a. Fretting b. Cavitation corrosion c. Creep d. Thermal shock stress e. Surface erosion Plastic deformation in a ductile machine element causing separation due to crack propagation a. Ductile rupture b. Fatigue c. Fretting d. Spalling 7) Static normal loads between two curved...
hep with question 3 please A material may fail in many ways; in a ductile or brittle mode; by creep or fatigue; by corrosion or stress corrosion; by hydrogen or liquid metal embrittlement; by slow tensile overload or by impact. An examination of the failure may tell you a lot about the material and the failure mode. In this course, you have learned (we trust) the correlations between structure-properties, - applications. This leads to material selection. However, the engineer has...
answer question 2 please A material may fail in many ways; in a ductile or brittle mode; by creep or fatigue; by corrosion or stress corrosion; by hydrogen or liquid metal embrittlement; by slow tensile overload or by impact. An examination of the failure may tell you a lot about the material and the failure mode. In this course, you have learned (we trust) the correlations between structure-properties, - applications. This leads to material selection. However, the engineer has to...
help with question 4 please. there are two samples given with two different pictures of each A material may fail in many ways; in a ductile or brittle mode; by creep or fatigue; by corrosion or stress corrosion; by hydrogen or liquid metal embrittlement; by slow tensile overload or by impact. An examination of the failure may tell you a lot about the material and the failure mode. In this course, you have learned (we trust) the correlations between structure-properties,...
help with question 5 please. there are two samples given with two different pictures of each. all of the information to solve is given A material may fail in many ways; in a ductile or brittle mode; by creep or fatigue; by corrosion or stress corrosion; by hydrogen or liquid metal embrittlement; by slow tensile overload or by impact. An examination of the failure may tell you a lot about the material and the failure mode. In this course, you...
Help 7.16 Started: Mar 13 at 11:30pm Quiz Instructions Question 1 1 pts Alarge flat plate is subjected to constant-amplitude uniaxial cyclic tensile stresses of a maximum stress of 102 and a minimum stress of 24 MPa. If before testing the largest surface crack is 0.61 mm and the plain-strain fracture toughness of the plate is 31.6 MPa m1/2 estimate the fatigue life of the plate in cycles to failure. For the plate, m - 4.2 and A = 5.0...
Consider 7075-T6 aluminum with fatigue crack growth in Table 16. Consider 7075-T6 aluminum with fatigue crack growth properties as given in Table 6.3. Assuming that 1=0.5 in the Walker equation, @. estimate da/dN versus AK equations in the form of Eq. 6.22a for R=0.4 and 0.8. 6. plot the equations from (a) on a log-log scale along with the R=0 equation. Keep in mind the proper region I limits of the equation. 169x10-5 ©. For a given AK, by what...
Question 17 1 pts What solubility properties are important in the selection of a solvent for recrystallisation? sparingly soluble in hot solvent and readily soluble in cold solvent readily soluble in both hot and cold solvent sparingly soluble in both hot and cold solvent readily soluble in hot solvent and sparingly soluble in cold solvent Question 18 1 pts How would you modify the procedure given in the Laboratory Manual if you did not know which solvent to use? if...