25 mmBrass coreE=105 GPa0 = 20.9 x 10 °CPROBLEM 2.49The aluminum shell is fully bonded to the brass core and theassembly is unstressed at a temperature of 15°C. Considering onlyaxial deformations, determine the stress in the aluminum when thetemperature reaches 195°C.60 mmAluminum shellE = 70 GPaa = 23.6 × 10°C

Answered: Image /qna-images/answer/4af32dc0-3220-4913-8afa-97fa828ebee0.jpg

Answered: 25 mm Brass core E = 105 GPa 0 = 20.9 x…

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

Similar questions

The assembly shown consists of an aluminum shell (E, = 70 GPa, az= 23.6 x 10-6PC) fully bonded to a steel core (Es= 200 GPa, as = 11.7 x 10 0rC) and the assembly is unstressed at a temperature of 20°C. Considering only axial deformations, determine the stress in the aluminum when the temperature reaches 210°C. 200 mm 20 mm Aluminum shell Steel 50 mm core The stress in the aluminum is |MPa.
The aluminum shell is fully bonded to the brass core, and the assembly is unstressed at a temperature of 78°F. The temperature of the assembly reaches 190°F. Consider only axial deformations. 1 in. -2.5 in. Brass core E = 15 x 106 psi a = 11.6 × 10-6°F Aluminum shell E = 10.6 × 106 psi a = 12.9 x 10-6°F Determine stress in the aluminum shell The stress in the aluminum shell is ____ksi.
show the FBD and complete solution
An 8-cm-square bar of steel is found to contain a1-mm corner crack, oriented perpendicular to the length ofthe bar. If an axial stress is applied from 0 to 420 MPa at afrequency of once every 10 minutes, how long will it take forthe rod to fracture? The properties of the bar are:KIC = 90 MPa √m , σys = 1500 MPa, and the crack growthrelation is da/dN = 2 x 10-37 ΔK4, with da/dN and ΔKbeing given in units of m/cycle and Pa √m , respectively
Which steel presents the maximum modulus of toughness UT? UT = ( (Sy − Sut) /2 ) ε f AISI 4142 and AISI 1020 AISI 1020 AISI 1095 and AISI 1020 AISI 4142 and AISI 1095
CEM BOGA 27°C Mostly sunny Q1. Determine the maximum strain energy that can be acquired by the composite rod ABC without causing any permanent deformations. Rod AB is made of a Structural Steel (ASTM- A36), rod BC is made of an Aluminum Alloy (2024-T4). A 1.5 m B 10-mm diameter Search 1.8 m 14-mm diameter 1/1 000 W 3
The assembly shown consists of an aluminum shell (E,= 70 GPa, az= 23.6 x 10-brC) fully bonded to a steel core (E= 200 GPa, a = 11.7 x 10 0rC) and the assembly is unstressed at a temperature of 20°C. Considering only axial deformations, determine the stress in the aluminum when the temperature reaches 205°C. 200 mm 20 mm Aluminum shell Steel 50 mm core The stress in the aluminum is MPa.
A steel structural member (E=30x106 psi, α=6.5x10-6/ºF in a furnace undergoes an increase in temperature of 95ºF while being held rigid at its ends. Determine the resulting stress, σ, in the steel. Looking to verify my answers! Thank you
The cold work is gevn for 15% then determine the upcoming values of its stength if the material is An annealed steel the properties of the material is Sy = 32.0 kpsi, Su = 49.5 kpsi,σf = 91.1 kpsi, σ0 = 90 kpsi, m = 0.25, and εf = 1.05 in/in. assume steel type :An annealed AISI 1018 steel please give detiled answer if expecting upvote
A part is subjected to uniaxial compression stress of 40 MPa in the x- direction ( -40MPA). If the material's elastic modulus (E) is 100 GPa and Poisson's ratio is 0.35. What are the strains in the y-direction and z- direction? Eyy = 0.00014, ɛ zz = 0.007 %3D O Eyy 0.00014, E zz 0.00014 Eyy = -0.00014, ɛ zz -0.00014 O Eyy -0.002, ɛzz = -0.006 %3| ||
The 50-mm-diameter cylinder is made from Am 1004-T61 magnesium and is placed in the clamp when the temperature is T₁ = 15°C. (Figure 1) Figure Part A 100 mm T₂ = Value If the two 304-stainless-steel carriage bolts of the clamp each have a diameter of 10 mm, and they hold the cylinder snug with negligible force against the rigid jaws, determine the temperature at which the average normal stress in either the magnesium or the steel first becomes 11.5 MPa. Express your answer to three significant figures and include the appropriate units. Units Submit Previous Answers Request Answer 150 mm ? 1 of 1
As shown in the figure, when the temperature was 24 ° C, a 0.5 mm gap was left. Determine the approximate value (° C) of the required temperature so that the normal stress in the aluminum bar is 75 MPa.

SEE MORE QUESTIONS

Recommended textbooks for you

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

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

SEE MORE TEXTBOOKS