4. The composite bar is initially stress-free. Calculate the stress in each material and indicate tension or compression if the temperature has increased to 25°C. Consider that the walls are unyielding and suitably braced to prevent buckling. Use 2 decimal places. 400 mm 800 mm 500 mm Aluminum A = 1400 mm? E = 75 GPa a = 23 x 10-6/°C Steel Bronze A = 800 mm² E = 200 GPa a = 10.7 x 10-6/°C A = 2500 mm? E = 85 GPa a = 19 x 10-6/°C 2

Materials Science And Engineering Properties
1st Edition
ISBN:9781111988609
Author:Charles Gilmore
Publisher:Charles Gilmore
Chapter12: Composite Materials
Section: Chapter Questions
Problem 12.7P: Estimate the transverse tensile strength of the concrete in Problem 12.6.
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4. The composite bar is initially stress-free. Calculate the stress in each material and indicate
tension or compression if the temperature has increased to 25°C. Consider that the walls are
unyielding and suitably braced to prevent buckling. Use 2 decimal places.
400 mm
800 mm
500 mm
Aluminum
A = 1400 mm?
E = 75 GPa
a = 23 x 10-6/°C
Steel
Bronze
A = 800 mm²
E = 200 GPa
a = 10.7 x 10-6/°C
A = 2500 mm?
E = 85 GPa
a = 19 x 10-6/°C
Transcribed Image Text:4. The composite bar is initially stress-free. Calculate the stress in each material and indicate tension or compression if the temperature has increased to 25°C. Consider that the walls are unyielding and suitably braced to prevent buckling. Use 2 decimal places. 400 mm 800 mm 500 mm Aluminum A = 1400 mm? E = 75 GPa a = 23 x 10-6/°C Steel Bronze A = 800 mm² E = 200 GPa a = 10.7 x 10-6/°C A = 2500 mm? E = 85 GPa a = 19 x 10-6/°C
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