Mechanics of Materials
11th Edition
ISBN: 9780137605460
Author: Russell C. Hibbeler
Publisher: Pearson Education (US)
expand_more
expand_more
format_list_bulleted
Concept explainers
Videos
Textbook Question
Chapter 10.6, Problem 39P
Determine the associated principal stresses at the point in the same plane. Eal = 10 (103) ksi, val = 0.33. Hint: See Prob.10−30.
Expert Solution & Answer
Want to see the full answer?
Check out a sample textbook solution
Students have asked these similar questions
Determine the required gap (δ) so that the rails just touch one another when the temperature is increased from Ti = -20F and Tf = 100F
Determine the stress in steel rails if the gap is δ = 0.5 in and the temperature is increased from Ti = -20F to Tf = 120F.
NOTE: indicate the free body diagram.
The A-36 steel pipe in (Figure 1) has a 6061-T6 aluminum core. It is
subjected to a tensile force of 200 kN. The pipe has an outer diameter
of 65 mm and an inner diameter of 55 mm. For A-36 steel,
Est = 200 GPa, and for 6061-T6 aluminum, E = 68.9 GPa.
Determine the average normal stress in the aluminum due to this loading.
Express your answer to three significant figures and include appropriate units.
?
Oal =
Value
Units
Submit
Request Answer
Part B
Determine the average normal stress in the steel due to this loading.
Express your answer to three significant figures and include appropriate units.
?
Figure
1 of 1
Value
Units
Ost =
400 mm
Submit
Request Answer
200 kN
200 kN
F14-8. Use Mohr's circle to determine the principal
stresses at the poinLAlso, find the corresponding arientation
of the element with respect to the element shown.
30 kPa
80 kPa
Chapter 10 Solutions
Mechanics of Materials
Ch. 10.3 - Prove that the sum of the normal strains in...Ch. 10.3 - The state of strain at the point on the arm has...Ch. 10.3 - The state of strain at the point on the leaf of...Ch. 10.3 - Use the strain transformation equations and...Ch. 10.3 - Determine the equivalent state of strain on an...Ch. 10.3 - Determine the equivalent state of strain which...Ch. 10.3 - Use the strain transformation equations to...Ch. 10.3 - Determine the equivalent state of strain, which...Ch. 10.3 - Solve Prob.103 using Mohrs circle. 103. The state...Ch. 10.5 - The strain at point A on the bracket has...
Ch. 10.5 - Determine (a) the principal strains at A, (b) the...Ch. 10.6 - For the case of plane stress, show that Hookes law...Ch. 10.6 - to develop the strain tranformation equations....Ch. 10.6 - Determine the associated principal stresses at the...Ch. 10.6 - Determine the applied load P. What is the shear...Ch. 10.6 - If a load of P = 3 kip is applied to the A-36...Ch. 10.7 - A material is subjected to plane stress. Express...Ch. 10.7 - A material is subjected to plane stress. Express...Ch. 10.7 - Solve Prob. 1061 using the maximum distortion...Ch. 10.7 - Solve Prob.1063 using the maximum distortion...Ch. 10.7 - Prob. 70PCh. 10.7 - The plate is made of Tobin bronze, which yields at...Ch. 10.7 - If a machine part is made of titanium (TI-6A1-4V)...Ch. 10.7 - The components of plane stress at a critical point...Ch. 10.7 - If Y = 50 ksi, determine the factor of safety for...Ch. 10.7 - Prob. 82PCh. 10.7 - If the yield stress for steel is Y = 36 ksi,...Ch. 10.7 - Prob. 84PCh. 10.7 - The state of stress acting at a critical point on...Ch. 10.7 - The shaft consists of a solid segment AB and a...Ch. 10 - In the case of plane stress, where the in-plane...Ch. 10 - The plate is made of material having a modulus of...Ch. 10 - If the material is machine steel having a yield...Ch. 10 - Determine if yielding has occurred on the basis of...Ch. 10 - The 60 strain rosette is mounted on a beam. The...Ch. 10 - Use the strain transformation equations to...Ch. 10 - If the strain gages a and b at points give...Ch. 10 - Use the strain-transformation equations and...Ch. 10 - Use the strain transformation equations to...Ch. 10 - Specify the orientation of the corresponding...
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
- бх бу 0 Txy στ Txy Oy In the diagram above, σ = 100 MPa, σ₁ = −27 MPa,, and Try = 40 MPa. Let each rotated plane within the stress cube be labelled by the angle that it makes relative to the original & plane. For this stress state, there is a set of planes which are in compression (σ < 0), and the corresponding values satisfy min < 0 < 0 max. If 0 is normalized to fall on [0°, 360°), what are the values of 0 min and @max ? Omin Өтах оarrow_forwardThe 510-kg engine is suspended from the jib crane at the position shown. (Figure 1) Figure 2m 2 m 2 m 430 D a 0.4 m 150 mm T 150 mm 20 mm- A 20 mm + T 300 mm 20 mm Section a-a 1 of 1 Part A Determine the normal stress at point A on the cross section of the boom at section a - a. Express your answer using three significant figures and include the appropriate units A= -3.327 Submit Previous Answers Request Answer Part B HÅ ^ * Incorrect; Try Again; 5 attempts remaining TA = Submit Determine the shear stress at point A. Express your answer to three significant figures and include the appropriate units. D Provide Feedback MPa μA Value Request Answer ? Units BE ?arrow_forwardFrom the figure as shown, determine the stress in psi at the top surface of the second cylinder. Assume the specific weight of the material is 460 Ibf/ft? F = 3000lbf d = 1 ft ww h = 1.5 ft wwarrow_forward
- Determine the state of stresses at point A.arrow_forwardDetermine the stress components acting on the inclined plane AB in (Figure 1), where τxy=−35.5MPa. Solve the problem using the stress transformation equations.arrow_forwardThe state of stress at a point in a member is shown on the element. Suppose that σx = -50MPa , σy = -120MPa , τxy = -30 MPa . Determine the normal stress component acting on the plane AB. σx′=?arrow_forward
- Determine the principal stresses, the maximum in-plane shear stress, and average normal stress. Specify the orientation of the element in each case.arrow_forwardDetermine the stress components acting on the inclined plane AB in (Figure 1), where τxy=−42.7MPa τxy=−42.7MPa. Solve the problem using the method of equilibrium.arrow_forwardQ 2: A cantilever beam has the profile shown so that it will provide sufficient clearances for large pulleys mounted on the line shaft its supports. The reaction of the line shaft is a load P-115.33KN. Determine the resultant normal stresses at the wall. 50 mm |20 - 120-arrow_forward
- Solve Prob. 9–7 using the stress transformation equations developed in Sec. 9.2.arrow_forwardroblem The two members are connected by two 20-mm bolts. If P = 10 kN, determine the normal and shear stresses in the bolts and the maximum bearing stress on the member. The nuts have an outer diameter of 30 mm. P P Guides to solve the problem: 12 mm Front view: 30° 1. Draw the FBD of one member. 2. Solve for the bearing force. 3. Section one bolt and solve internal forces. 4. Solve for the normal and shear stress in the bolts. 5. Solve for the bearing stress in the members due to the nuts. 6. Solve for the bearing stress in the members due to the bolts. 36 mm 36 mm P Parrow_forwardThe state of stress at a point in a member is shown on the element. Take σx = 90 MPa , σy= 65 MPa , τxy = 40 MPa . A) Determine the normal stress component acting on the inclined plane AB. Solve the problem using the method of equilibrium. B)Determine the shear stress component acting on the inclined plane AB. Solve the problem using the method of equilibrium.arrow_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 Press
Mechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSON
Thermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEY
Mechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage Learning
Engineering 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
Everything About COMBINED LOADING in 10 Minutes! Mechanics of Materials; Author: Less Boring Lectures;https://www.youtube.com/watch?v=N-PlI900hSg;License: Standard youtube license