Using the table below, estimate the components of the matrices and develop the stiffness and compliance matrices for an orthotropic lamina of E-glass/470-36 E-glass/vinylester.
Using the table below, estimate the components of the matrices and develop the stiffness and compliance matrices for an orthotropic lamina of E-glass/470-36 E-glass/vinylester.
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
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- Using the table below, estimate the components of the matrices and develop the stiffness and compliance matrices for an orthotropic lamina of E-glass/470-36 E-glass/vinylester.
![Typical Values of Lamina Engineering Constants for Several Composites Having
Fiber Volume Fraction uf (Principles of Composite Material Mechanics 4th Edition Ronald F. Gibson)
Material
T300/934 carbon/epoxy
AS/3501 carbon/epoxy
P-100/ERL 1962 pitch/
carbon/epoxy
IM7/8551-7 carbon/
toughened epoxy
AS4/APC2 carbon/PEEK
Boron/6061 boron/
O aluminum
IM
Kevlar 49/934 aramid/
epoxy
Scotchply 1002 E-glass/
epoxy
IM
Boron/5505 boron/epoxy
Spectra 900/826
polyethylene/epoxy
E-glass/470-36 E-glass/
vinylester
E, [Msi (GPa)]
19.0 (131)
20.0 (138)
68.0 (468.9)
23.5 (162)
19.1 (131)
34.1 (235)
11.0 (75.8)
5.6 (38.6)
29.6 (204.0)
4.45 (30.7)
3.54 (24.4)
E₂ [Msi (GPa)]
1.5 (10.3)
1.3 (9.0)
0.9 (6.2)
1.21 (8.34)
1.26 (8.7)
19.9 (137)
0.8 (5.5)
1.2 (8.27)
2.68 (18.5)
0.51 (3.52)
1.0 (6.87)
G₁₂ [Msi (GPa)]
1.0 (6.9)
1.0 (6.9)
0.81 (5.58)
0.3 (2.07)
0.73 (5.0)
6.8 (47.0)
0.33 (2.3)
0.6 (4.14)
0.81 (5.59)
0.21 (1.45)
0.42 (2.89)
V₁2 U₁
0.22 0.65
0.3 0.65
0.31 0.62
0.34 0.6
0.28 0.58
0.3 0.5
0.34 0.65
0.26 0.45
0.23 0.5
0.32 0.65
0.32 0.30
Note: Kevlar is a registered trademark of DuPont Company, Wilmington, Delaware; Scotchply™ is a
registered trademark of 3M Company, St. Paul, Minnesota; and Spectra is a registered
trademark of Honeywell International, Inc.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F5c944c72-4310-40fb-aea7-bf5588c25c1b%2F763d9120-b63a-4cc5-a07b-ec2a477de23e%2F0r3q2bk_processed.png&w=3840&q=75)
Transcribed Image Text:Typical Values of Lamina Engineering Constants for Several Composites Having
Fiber Volume Fraction uf (Principles of Composite Material Mechanics 4th Edition Ronald F. Gibson)
Material
T300/934 carbon/epoxy
AS/3501 carbon/epoxy
P-100/ERL 1962 pitch/
carbon/epoxy
IM7/8551-7 carbon/
toughened epoxy
AS4/APC2 carbon/PEEK
Boron/6061 boron/
O aluminum
IM
Kevlar 49/934 aramid/
epoxy
Scotchply 1002 E-glass/
epoxy
IM
Boron/5505 boron/epoxy
Spectra 900/826
polyethylene/epoxy
E-glass/470-36 E-glass/
vinylester
E, [Msi (GPa)]
19.0 (131)
20.0 (138)
68.0 (468.9)
23.5 (162)
19.1 (131)
34.1 (235)
11.0 (75.8)
5.6 (38.6)
29.6 (204.0)
4.45 (30.7)
3.54 (24.4)
E₂ [Msi (GPa)]
1.5 (10.3)
1.3 (9.0)
0.9 (6.2)
1.21 (8.34)
1.26 (8.7)
19.9 (137)
0.8 (5.5)
1.2 (8.27)
2.68 (18.5)
0.51 (3.52)
1.0 (6.87)
G₁₂ [Msi (GPa)]
1.0 (6.9)
1.0 (6.9)
0.81 (5.58)
0.3 (2.07)
0.73 (5.0)
6.8 (47.0)
0.33 (2.3)
0.6 (4.14)
0.81 (5.59)
0.21 (1.45)
0.42 (2.89)
V₁2 U₁
0.22 0.65
0.3 0.65
0.31 0.62
0.34 0.6
0.28 0.58
0.3 0.5
0.34 0.65
0.26 0.45
0.23 0.5
0.32 0.65
0.32 0.30
Note: Kevlar is a registered trademark of DuPont Company, Wilmington, Delaware; Scotchply™ is a
registered trademark of 3M Company, St. Paul, Minnesota; and Spectra is a registered
trademark of Honeywell International, Inc.
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