Homework Help is Here – Start Your Trial Now!
Engineering
Mechanical Engineering
A single edge-cracked plate of AISI 4130 Steel of Table 8.1 has dimensions, as defined in Fig 8.12(c), of b = 45 mm and t = 5.0 mm, (large h), and is subjected to a tension force of P = 81 kN. Inspection of the plate shows crack length a = 4.5 mm. a. Determine the safety factor against brittle fracture, Xk. b. Determine the safety factor against fully plastic yielding, X'o. c. Determine the safety factor on crack length, Xa

A single edge-cracked plate of AISI 4130 Steel of Table 8.1 has dimensions, as defined in Fig 8.12(c), of b = 45 mm and t = 5.0 mm, (large h), and is subjected to a tension force of P = 81 kN. Inspection of the plate shows crack length a = 4.5 mm. a. Determine the safety factor against brittle fracture, Xk. b. Determine the safety factor against fully plastic yielding, X'o. c. Determine the safety factor on crack length, Xa

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
See similar textbooks
icon
Related questions
Question

A single edge-cracked plate of AISI 4130 Steel of Table 8.1 has dimensions, as defined in Fig 8.12(c), of b = 45 mm and t = 5.0 mm, (large h), and is subjected to a tension force of P = 81 kN. Inspection of the plate shows crack length a = 4.5 mm.
a. Determine the safety factor against brittle fracture, Xk.
b. Determine the safety factor against fully plastic yielding, X'o.
c. Determine the safety factor on crack length, Xa.

Problem 2: Equations, Tables, and Figures Table 8.1 Fracture Toughness and Corresponding Tensile Properties for Representative Metals at Room Temperature Toughness Kie Material (a) Steels AISI 1144 ASTM A470-8 (Cr-Mo-V) ASTM A517-F AISI 4130 18-Ni maraging air melted 18-Ni maraging vacuum melted 300-M 650° C temper 300-M 300 C temper 2014-T651 2024-T351 2219-T851 7075-T651 7475-T7351 Ti-6Al-4V MPa m (ksivin) annealed 66 (60) 60 (55) 187 (170) 110 (100) POSROT 123 (112) 176 (160) 152 (138) 65 (59) 24 (22) 34 (31) 36 (33) 29 (26) 52 (47) Yield Ultimate Elong. Red. Area 100g/ RA On σo % 66 (60) MPa (ksi) 540 (78) 620 (90) 760 (110) 1090 (158) 1310 (190) (b) Aluminum and Titanium Alloys (L-T Orientation) 415 485 (60) 1290 (187) 1070 (156) 1740 (252) 325 (47) 505 (73) 435 MPa (ksi) (63) 840 (122) 200 925 (134) 780 (113) 830 (121) 1150 (167) 1350 (196) 1345 (195) 1190 (172) 2010 (291) 350 455 (51) (66) (70) 470 (68) 570 (83) 505 (73) 1000 (145) 5 17 20 14 12 15 18 12 13 20 10 14 16 7.0 45 66 49 54 66 56 48 34 Sources: Data in [Barsom 87] p. 172. [Boyer 85] pp. 6.34. 6.35. and 9.8. [MILIDBK 94] pp. 3.10 3.12 and 5.3. and [Ritchie 77] I meldean
Transcribed Image Text:Problem 2: Equations, Tables, and Figures Table 8.1 Fracture Toughness and Corresponding Tensile Properties for Representative Metals at Room Temperature Toughness Kie Material (a) Steels AISI 1144 ASTM A470-8 (Cr-Mo-V) ASTM A517-F AISI 4130 18-Ni maraging air melted 18-Ni maraging vacuum melted 300-M 650° C temper 300-M 300 C temper 2014-T651 2024-T351 2219-T851 7075-T651 7475-T7351 Ti-6Al-4V MPa m (ksivin) annealed 66 (60) 60 (55) 187 (170) 110 (100) POSROT 123 (112) 176 (160) 152 (138) 65 (59) 24 (22) 34 (31) 36 (33) 29 (26) 52 (47) Yield Ultimate Elong. Red. Area 100g/ RA On σo % 66 (60) MPa (ksi) 540 (78) 620 (90) 760 (110) 1090 (158) 1310 (190) (b) Aluminum and Titanium Alloys (L-T Orientation) 415 485 (60) 1290 (187) 1070 (156) 1740 (252) 325 (47) 505 (73) 435 MPa (ksi) (63) 840 (122) 200 925 (134) 780 (113) 830 (121) 1150 (167) 1350 (196) 1345 (195) 1190 (172) 2010 (291) 350 455 (51) (66) (70) 470 (68) 570 (83) 505 (73) 1000 (145) 5 17 20 14 12 15 18 12 13 20 10 14 16 7.0 45 66 49 54 66 56 48 34 Sources: Data in [Barsom 87] p. 172. [Boyer 85] pp. 6.34. 6.35. and 9.8. [MILIDBK 94] pp. 3.10 3.12 and 5.3. and [Ritchie 77] I meldean
F 6 5 4 3 2 L 0 P Equations, Tables, and Figures 11 Sg (a) K = FSg√πa P Sg=2bt P Sg= bt Figure 8.12 (b) b 0.2 (a) F = h (a, b) (c) 0.4 Values for small a/b and limits for 10% accuracy: (a) K = S₂√√ña (a/b ≤ 0.4) Expressions for any a = alb: b a = a/b h (c) F = 0.265 (1-x)² + 1 -0.5a +0.326x² √1-a CX 2 (b) F = (1 +0.122 cos+ 2)√ (c) (b) K = 1.12S √√а 0.6 (a/b ≤0.6) 12 tan πα 0.857 +0.265a (1-a)³/2 (c) a|- TO 0.8 h -- (c) K = 1.12S√√ла 1.0 (a/b ≤0.13) 1 1094 (107) (h/b> 1.5) (h/b> 2) (h/b≥ 1)
Transcribed Image Text:F 6 5 4 3 2 L 0 P Equations, Tables, and Figures 11 Sg (a) K = FSg√πa P Sg=2bt P Sg= bt Figure 8.12 (b) b 0.2 (a) F = h (a, b) (c) 0.4 Values for small a/b and limits for 10% accuracy: (a) K = S₂√√ña (a/b ≤ 0.4) Expressions for any a = alb: b a = a/b h (c) F = 0.265 (1-x)² + 1 -0.5a +0.326x² √1-a CX 2 (b) F = (1 +0.122 cos+ 2)√ (c) (b) K = 1.12S √√а 0.6 (a/b ≤0.6) 12 tan πα 0.857 +0.265a (1-a)³/2 (c) a|- TO 0.8 h -- (c) K = 1.12S√√ла 1.0 (a/b ≤0.13) 1 1094 (107) (h/b> 1.5) (h/b> 2) (h/b≥ 1)
Expert Solution
trending now

Trending now

This is a popular solution!

steps

Step by step

Solved in 5 steps with 4 images

SEE SOLUTIONCheck out a sample Q&A here
Blurred answer
Knowledge Booster
Types of Properties of Engineering Materials
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Similar questions
  • SEE MORE QUESTIONS
Recommended textbooks for you
Elements Of Electromagnetics
Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Control Systems Engineering
Control Systems Engineering
Mechanical Engineering
ISBN:
9781118170519
Author:
Norman S. Nise
Publisher:
WILEY
Mechanics of Materials (MindTap Course List)
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:
9781337093347
Author:
Barry J. Goodno, James M. Gere
Publisher:
Cengage Learning
Engineering Mechanics: Statics
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:
9781118807330
Author:
James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:
WILEY
SEE MORE TEXTBOOKS