Homework Help is Here – Start Your Trial Now!
Engineering
Mechanical Engineering
An aluminum bar (6061-T4) is initially 250.00 mm long at a temperature of 50°C. It is placed between two immovable end plates that are 260.00 mm apart. The gap between the bar and the two end plates is 1.0 mm. Determine the final temperature at which the gap between the bar and the two immovable end plates becomes 0.4 mm. Thermal expansion coefficient of aluminum is 23.4 x 106 C. End Bar End Plate Plate Gap 3.

An aluminum bar (6061-T4) is initially 250.00 mm long at a temperature of 50°C. It is placed between two immovable end plates that are 260.00 mm apart. The gap between the bar and the two end plates is 1.0 mm. Determine the final temperature at which the gap between the bar and the two immovable end plates becomes 0.4 mm. Thermal expansion coefficient of aluminum is 23.4 x 106 C. End Bar End Plate Plate Gap 3.

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
Added the table in case if it’s needed
MT345 %20%232_211122.pdf 4 / 8 100% 3. An aluminum bar (6061-T4) is initially 250.00 mm long at a temperature of 50°C. It is placed between two immovable end plates that are 260.00 mm apart. The gap between the bar and the two end plates is 1.0 mm. Determine the final temperature at which the gap between the bar and the two immovable end plates becomes 0.4 mm. Thermal expansion coefficient of aluminum is 23.4 x 106 C'. End Bar End Plate Plate → - Gap NOV 22 étv A Aa
Transcribed Image Text:MT345 %20%232_211122.pdf 4 / 8 100% 3. An aluminum bar (6061-T4) is initially 250.00 mm long at a temperature of 50°C. It is placed between two immovable end plates that are 260.00 mm apart. The gap between the bar and the two end plates is 1.0 mm. Determine the final temperature at which the gap between the bar and the two immovable end plates becomes 0.4 mm. Thermal expansion coefficient of aluminum is 23.4 x 106 C'. End Bar End Plate Plate → - Gap NOV 22 étv A Aa
7 / 8 91% + | 日の - A-14 Typical properties of aluminum alloys." Ultimate strength, s, Yield strength, s, Shear strength, sus Alloy and temper Percent ksi MPa ksi MPa elongation ksi MPa Alloys in wrought form 16 1100-H12 110 15 103 25 10 69 1100-H18 24 165 22 152 15 13 90 2014-0 27 186 14 97 18 18 124 2014-T4 62 427 42 290 20 38 262 2014-T6 70 483 60 414 13 42 290 3003-0 16 110 6 41 40 11 76 3003-H12 19 131 18 124 20 12 83 3003-H18 29 200 27 186 10 16 110 5154-0 35 241 17 117 27 22 152 5154-H32 39 269 30 207 15 22 152 5154-H38 48 331 39 269 10 28 193 6061-0 18 124 8. 55 30 12 83 6061-T4 35 241 21 145 25 24 165 6061-T6 45 310 40 276 17 30 207 7075-0 33 228 15 103 16 22 152 7075-T6 83 572 73 503 11 48 331 Casting alloys-permanent mold castings 204.0-T4 48 331 29 200 206.0-T6 65 445 59 405 356.0-T6 41 283 30 207 10 *Modulus of elasticity E varies for different aluminum alloys: For most alloys, including 1100, 3003, 6061, 6063, E = 10 x 10 psi (69.0 GPa). For alloy 2014, E = 10.6 x 10 psi (73.1 GPa). For alloy 5154, E = 10.2 x 10 psi (70.3 GPa). For alloy 7075, E =10.4 x 10 psi (71.7 GPa). Density of most aluminum alloys is approximately 0.100 lb /in. (2770 kg/m). NOV 22 A Aa tv | ||
Transcribed Image Text:7 / 8 91% + | 日の - A-14 Typical properties of aluminum alloys." Ultimate strength, s, Yield strength, s, Shear strength, sus Alloy and temper Percent ksi MPa ksi MPa elongation ksi MPa Alloys in wrought form 16 1100-H12 110 15 103 25 10 69 1100-H18 24 165 22 152 15 13 90 2014-0 27 186 14 97 18 18 124 2014-T4 62 427 42 290 20 38 262 2014-T6 70 483 60 414 13 42 290 3003-0 16 110 6 41 40 11 76 3003-H12 19 131 18 124 20 12 83 3003-H18 29 200 27 186 10 16 110 5154-0 35 241 17 117 27 22 152 5154-H32 39 269 30 207 15 22 152 5154-H38 48 331 39 269 10 28 193 6061-0 18 124 8. 55 30 12 83 6061-T4 35 241 21 145 25 24 165 6061-T6 45 310 40 276 17 30 207 7075-0 33 228 15 103 16 22 152 7075-T6 83 572 73 503 11 48 331 Casting alloys-permanent mold castings 204.0-T4 48 331 29 200 206.0-T6 65 445 59 405 356.0-T6 41 283 30 207 10 *Modulus of elasticity E varies for different aluminum alloys: For most alloys, including 1100, 3003, 6061, 6063, E = 10 x 10 psi (69.0 GPa). For alloy 2014, E = 10.6 x 10 psi (73.1 GPa). For alloy 5154, E = 10.2 x 10 psi (70.3 GPa). For alloy 7075, E =10.4 x 10 psi (71.7 GPa). Density of most aluminum alloys is approximately 0.100 lb /in. (2770 kg/m). NOV 22 A Aa tv | ||
Expert Solution
steps

Step by step

Solved in 2 steps with 2 images

SEE SOLUTIONCheck out a sample Q&A here
Blurred answer
Knowledge Booster
Buckling of Columns
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.
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