Compute the expected properties of ultimate strength (Suc) of a composite made from S-glass fibers and an epoxy matrix. The volume fraction of fibers is 30%. (Unit is psi.) Properties of Sample Matrix and Filler Materials Tensile strength Tensile modulus Specific weight ksi MPa 10 psi GPa Ibin kN/m Matrix materials: Polycster Ероху Aluminum Titanium 10 69 0.40 2.76 0.047 12.7 18 124 0.56 3.86 * 69 0.047 12.7 45 310 10.0 16.5 0.100 27.1 170 1170 114 0.160 43.4 iller materials: S-glass Carbon-PAN Carbon-PAN (high-strength) Carbon (high-modulus) 600 4140 3240 5650 2200 3450 12.5 86.2 231 276 0.09 0.064 0.065 24.4 470 33.5 40 17.4 820 325 17.7 100 690 0.078 21.2 Aramid 500 19.0 131 0.052 14.1
Compute the expected properties of ultimate strength (Suc) of a composite made from S-glass fibers and an epoxy matrix. The volume fraction of fibers is 30%. (Unit is psi.) Properties of Sample Matrix and Filler Materials Tensile strength Tensile modulus Specific weight ksi MPa 10 psi GPa Ibin kN/m Matrix materials: Polycster Ероху Aluminum Titanium 10 69 0.40 2.76 0.047 12.7 18 124 0.56 3.86 * 69 0.047 12.7 45 310 10.0 16.5 0.100 27.1 170 1170 114 0.160 43.4 iller materials: S-glass Carbon-PAN Carbon-PAN (high-strength) Carbon (high-modulus) 600 4140 3240 5650 2200 3450 12.5 86.2 231 276 0.09 0.064 0.065 24.4 470 33.5 40 17.4 820 325 17.7 100 690 0.078 21.2 Aramid 500 19.0 131 0.052 14.1
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
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Answer whats in the image, please and thank you

Transcribed Image Text:Compute the expected properties of ultimate strength (Suc) of a composite made from S-glass fibers and an epoxy matrix. The
volume fraction of fibers is 30%. (Unit is psi.)
Properties of Sample Matrix and Filler Materials
Tensile strength
Tensile modulus
Specific weight
ksi
MPa
10 psi
GPa
bin
IN/m
Matrix materials:
Polycster
Ероху
Aluminum
10
69
0.40
2.76
0.047
12.7
18
124
0.56
3.86
0.047
12.7
45
310
10.0
* 69
0.100
27.1
Titanium
170
1170
16.5
114
0.160
43.4
Filler materials:
S-glass
Carbon-PAN
600
4140
3240
5650
2200
12.5
86.2
0.09
0.064
24.4
470
33.5
40
231
276
690
17.4
Carbon-PAN (high-strength)
Carbon (bigh-modulus)
820
0.065
17.7
325
100
0.078
21.2
Aramid
500
3450
19.0
131
0.052
14.1
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