A long metal plate (E = 210 GPa) with some cutouts in it is mounted between two rigid plates at 6 am. By noon, the temperature has risen by 20°C. The structure is made from aluminium with a coefficient of thermal expansion of a = 23 x 10-6/°C. Please use the stress concentration chart shown below for any relevant calculations. a10 h L O Use the following values in your working out: K 3.2 3.0 2.8 2.6 2.4 2.2 2.0 L = 13 m h = 5.3 m a = 0.8 m b = 1.6 m 0 0.1 W PA 0.2 W Javg = 0.3 2r P (w2r)t 0.4 P 0.5 a) What is the average normal stress throughout the plate at noon? b) What is the maximum stress at any point in the structure? c) The material the plate is made from has a tensile yield stress of 416 MPa and a compressive yield stress of 200 MPa. Using these values, do you expect the plate to yield at/before noon?

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
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A long metal plate (E = 210 GPa) with some cutouts in it is mounted between two rigid plates at 6 am. By noon, the temperature
has risen by 20°C. The structure is made from aluminium with a coefficient of thermal expansion of a = 23 x 10-6/°C.
Please use the stress concentration chart shown below for any relevant calculations.
a10
h
L
b
O
Use the following values in your working out:
K
3.2
3.0
2.8
2.6
2.4
2.2
2.0
L = 13 m
0
0.1
P
0.2
W
W
Javg
0.3
2r
P
(w2r)t
0.4
P
▬▬▬▬▬▬▬
0.5
h = 5.3 m
a = 0.8 m
b = 1.6 m
a) What is the average normal stress throughout the plate at noon?
b) What is the maximum stress at any point in the structure?
c)
The material the plate is made from has a tensile yield stress of 416 MPa and a compressive yield stress of 200 MPa. Using
these values, do you expect the plate to yield at/before noon?
Transcribed Image Text:A long metal plate (E = 210 GPa) with some cutouts in it is mounted between two rigid plates at 6 am. By noon, the temperature has risen by 20°C. The structure is made from aluminium with a coefficient of thermal expansion of a = 23 x 10-6/°C. Please use the stress concentration chart shown below for any relevant calculations. a10 h L b O Use the following values in your working out: K 3.2 3.0 2.8 2.6 2.4 2.2 2.0 L = 13 m 0 0.1 P 0.2 W W Javg 0.3 2r P (w2r)t 0.4 P ▬▬▬▬▬▬▬ 0.5 h = 5.3 m a = 0.8 m b = 1.6 m a) What is the average normal stress throughout the plate at noon? b) What is the maximum stress at any point in the structure? c) The material the plate is made from has a tensile yield stress of 416 MPa and a compressive yield stress of 200 MPa. Using these values, do you expect the plate to yield at/before noon?
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