Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering)
10th Edition
ISBN: 9780073398204
Author: Richard G Budynas, Keith J Nisbett
Publisher: McGraw-Hill Education
expand_more
expand_more
format_list_bulleted
Concept explainers
Textbook Question
Chapter 1, Problem 14P
Determinations of the ultimate tensile strength Swt of stainless-steel sheet (17-7PH, condition TH 1050), in sizes from 0.016 to 0.062 in. in 197 tests combined into seven classes were
Swt (kpsi) | | 174 | 182 | 190 | 198 | 206 | 214 | 222 |
f | 6 | 9 | 44 | 67 | 53 | 12 | 6 |
where Swt is the class midpoint and f is the class frequency. Estimate the mean and standard deviation.
Expert Solution & Answer
Want to see the full answer?
Check out a sample textbook solutionStudents have asked these similar questions
The endurance limit for a material is found by rotating beam specimen test to be S,' = 52 kpsi. Using a reliability estimate of 99.9 percent, estimate the endurance limit if the material is to be placed in reversed axial loading.
Table 6-4 Reliability Factors k, Corresponding to 8 Percent Standard
Deviation of the Endurance Limit
Reliability, %
Transformation Variate z.
Reliability Factor k,
50
1.000
90
1.288
0.897
95
1.645
0.868
99
2.326
0.814
99.9
3.091
0.753
99.99
3.719
0.702
The following data was obtained from a tensile test on
Load (kN)
16
32
56
72
95
110
132
142
140
135
Extension (mm)
0.2
0.4
0.7
0.9
1.5
2.5
5.0
8,5
10.0
12.0
a specimen of 10mm diameter and gauge length 60mm.
Using the graph paper supplied, plot the load-extension
diagram and determine:
(1) The tensile strength
(2) 0.1% Proof Stress
(3) Young's Modulus for the specimen
Asiacell 4,ll
ON 76%
D19:17
سؤال الواجب.docx
Problem :-
The following data was obtained tensile test on a specimen of 6 mm diameter and
gauge length Lo=30 mm:
load(KN)
0 40
80
95
90
135
150.2 145 130 120
elongation(mm) 0 0.022 0.13 0.25 0.55 2.01 3.88
4.12 5.22 6
Plot engineering and True (stress-strain) curves, then determine the (oy, ɛy), (ou,
ɛu), (of, , ef), ductility , modulus of elasticity .
Then select on the drawing (strain hardening (n)), (Necking), (uniform plastic
region and non-uniform plastic region) and (elastic & plastic) region)?
Chapter 1 Solutions
Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering)
Ch. 1 - Select a mechanical component from Part 3 of this...Ch. 1 - Select a mechanical component from Part 3 of this...Ch. 1 - Select an organization listed in Sec. 16, go to...Ch. 1 - Go to the Internet and connect to the NSPE website...Ch. 1 - Go to the Internet and connect to the NSPE website...Ch. 1 - Estimate how many times more expensive it is to...Ch. 1 - The costs to manufacture a part using methods A...Ch. 1 - A cylindrical part of diameter d is loaded by an...Ch. 1 - When one knows the true values x1 and x2 and has...Ch. 1 - Use the true values x1 = 7 and x2 = 8 (a)...
Ch. 1 - A solid circular rod of diameter d undergoes a...Ch. 1 - A fatigue test is performed on rotating beam...Ch. 1 - Determinations of the ultimate tensile strength...Ch. 1 - The lives of parts are often expressed as the...Ch. 1 - The tensile 0.2 percent offset yield strength of...Ch. 1 - A mechanical system comprises three subsystems in...Ch. 1 - From See. 3-12, the maximum shear stress in a...Ch. 1 - A round cold-drawn 1045 steel rod has a mean...Ch. 1 - A beam subjected to axial loading will experience...Ch. 1 - Three blocks A, B, and C and a grooved block D...Ch. 1 - The volume of a rectangular parallelepiped is...Ch. 1 - A pivot in a linkage has a pin in the figure whose...Ch. 1 - A circular cross section O ring has the dimensions...Ch. 1 - Prob. 25PCh. 1 - Prob. 26PCh. 1 - Prob. 27PCh. 1 - Prob. 28PCh. 1 - Convert the following to appropriate ips units:...Ch. 1 - Convert the following to appropriate SI units: (a)...Ch. 1 - Generally, final design results are rounded to or...Ch. 1 - Repeal Prob. 1-31 for the following: (a) = F/wt,...Ch. 1 - Repeat Prob. 131 for: (a) = F/A, where A = d2/4, F...
Knowledge Booster
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
- Parrow_forwardA tensile test was performed to find the stress-strain curve of a metal sample.Here are the results provided by the tensile testing machine.Suppose the results are free of errors. Elongation, 0 AL (cm) Applied force , F(N) 4.086 5.448 2.724 6.81 1.362 55571.1 61710.1 52930.5 68018.1 39498.3 Additional information : Lo : the length of the extensometer Lo = 5.42 cm A= 5.342 Questions : a) At. Using the 0.2% yield strength method, calculate the tensile strength of the metal sample. b) Find the modulus of resilience of the material under test. c) Calculate the allowable load for an object made of this metal using the parameters following: * Maximum stress: elastic limit Cross section: 10 mm2 Safety factor (or margin): 7 Calculate numerically with a minimum of four decimal places.arrow_forwardYou have been given the following set of data from a soil-geotextile friction test: Normal stress (kPa) Peak shear strength (kPa) Residual shear strength (kPa) 17 20.2 13 35 31 22 70 52 39.5 140 94 74.5 (a) Plot the Mohr-Coulomb failure envelope (x-axis=normal stress; y-axis=shear stress) (b) Determine the peak friction angle, and the residual friction angle, . (c) Determine the peak adhesion and the residual adhesion. (d) Calculate the fabric efficiency based on a soil friction angle of = 35-degrees using the peak friction angle. **HINT: the equation for efficiency of soil friction angle mobilization is:arrow_forward
- During a tensile test of Aluminum alloy whose initial diameter was 0.505-in and gage length was 2.0-in, the following data was recorded. Load Elongation (in.) Load Elongation (in.) 0.020 (1b) |(Ib) 14 000 2 310 0.00220 14 400 0.025 4 640 0.00440 14 500 0.060 6 950 0.00660 14 600 0.080 9 290 0.00880 14 800 0.100 11 600 0.0110 14 600 0.120 12 600 0.0150 13 600 Fracture a) Determine Stress and strain b) Draw the stress strain diagram c) Determine the following mechanical properties 1) Proportional limit, 2) Modulus of elasticity 3) Yield point 4) Ultimate strength 5) Rupture strength.arrow_forwardThe shear modulus. G. of a material can be determined by applying a torque. T, on a cylindrical material specimen and measuring the angular twist, 0. The modulus can then be calculated from: G each measured variable (L. T.t. 0, R) is 3.4%. 3LT 2 Ree where R and Lare the specimen radius and length, respectively. The relative uncertainty in What is the total relative uncertainty in G? (Provide your amwer as a percentage using two decimal places. Do not include the % symbol.) 1226arrow_forwardThe following data were recorded during the tensile test of a 12.8 mm diameter stainless steel rod. The gauge length was 50.8 mm. Load Length Load Length N N 50.800 107.800 51.308 50.825 119,400 51.562 128,300| 51.816 149,700 52.832 50.902 159,000 53.848 160,400 54.356 159,500 54.864 151,500 55.880 124,700 56.642 mm mm 12,700 25,400 38,100 50,800 76,200 89,100 92,700 102,500 | 51.181 50.851 50.876 50.952 51.003 51.054arrow_forward
- 16:57 A steel specimen has an original diameter of 0.503 and gage length of 2. You perform a tensile test and acquire the following data: Load (kN) 0 1.5 4.6 8 wamap.org 11 11.8 11.8 12 16.6 20 21.5 19.5 18.5 Elongation (m) 0 0.0005 0.0015 0.0025 0.0035 0.005 0.008 0.02 0.04 0.1 0.28 0.4 0.46 a. Plot the stress-strain diagram on EXCEL (or write MATLAB code to generate the plot). a. Do not calculate stress and strain by hand. In Excel use the function tool: Load (kip Elongation (in) 0 0 1.51 4.6 0.0005 0.0015 Stress Strain 0 =A4/$A$19 23.149 0.00075 If you are using MATLAB, write code to calculate stress and strain. b. Label the x- and y-axes and include units c. Include your name in the filename d. Upload to CANVAS b. Determine the Elastic Modulus, E. c. Read the yield stress off the graph, σy. d. Read the ultimate stress off the graph, ou. e. Read the fracture stress off the graph, of. Round your final answers to 3 significant digits/figures. 1. upload your EXCEL file (or MATLAB…arrow_forwardmechaarrow_forwardThe following data were recorded during the tensile test of a 12.8 mm diameter stainless steel rod. The gauge length was 50.8 mm. Load Length Load Length mm mm 107.800 51.308 119,400 51.562 128,300 51.816 149,700| 52.832 50.800 50.825 12,700 25.400 50.851 38,100 50.876 50,800 76,200 89,100 92,700 102,500 51.181 124,700 56.642 50.902 50.952 159,000 53.848 160,400| 54.356 159,500 54.864 51.054 151,500 55.880 51.003 using the data above plot the stress-strain diagram and determine the following mechanical properties Q1 The proportional limit Q 2 The modulus of elasticity Q 3 yield point Q5 The Últimate Tensile Strength Q 4 yield strength at 0.2% offset Q 6 rupture strengtharrow_forward
- Tutorial Mechanical properties 1. Based on data collected as Table 1, plot graph Stress vs strain, determine YS, TS and E. | Table 1: Data load and length for tensile test Gage length (mm) Load Gage length Load (N) (mm) (N) 35,220 35,720 40,540 50.8000 50.9778 50.8102 50.8203 4,890 51.0032 9,779 51.8160 14,670 50.8305 48,390 53.3400 19,560 24,450 27,620 29,390 32,680 33.950 34,580 50.8406 59,030 65,870 69,420 69,670 (maximum) 55.8800 50.8508 50.8610 58.4200 60.9600 50.8711 61.4680 50.9016 68,150 63.5000 50.9270 60,810 (fracture) 66.0400 (after fracture) 50.9524 Original, specimen diameter: 12.7 mm.arrow_forwardA 1045 hot-rolled steel tension test specimen has the original diameter and length of 6 mm and 25 mm, respectively. The load and change in length data were recorded as shown in Table 1 below: Table 1. Load and change in length Load (KN) Change in Length Load (KN) Change in Length (mm) |(mm) 20.56 2.26 2.94 0.01 20.72 3.36 5.58 0.02 20.61 3.83 8.52 0.03 19.97 4.00 11.16 0.04 18.72 Fracture. 12.63 0.05 13.02 0.06 13.16 0.08 13.22 0.10 16.15 0.61 18.50 1.04 20.27 1.80arrow_forwardGraph the following data on a stress-strain curve. Identify/Determine the following: Elastic Limit, Plastic Limit, Proportional Limit, Upper Yield Point, Lower Yield Point, Ultimate Strength, Rupture Strength, and Modulus of Elasticity. Engr. True Stress Strain o, MPa 102.3 0.00050 204.7 0.00102 293.5 0.00146 272.9 0.00230 264.0 0.00310 268.9 0.00500 267.6 0.00700 264.0 0.01000 318.6 0.0490 372.0 0.1250 394.4 0.2180 395.0 0.2340 384.2 0.3060 360.4 0.3300 327.5 0.3480 290.0 0.3600 266.8 0.3660arrow_forward
arrow_back_ios
SEE MORE QUESTIONS
arrow_forward_ios
Recommended textbooks for you
- 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
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY
How Shell and Tube Heat Exchangers Work (Engineering); Author: saVRee;https://www.youtube.com/watch?v=OyQ3SaU4KKU;License: Standard Youtube License