Engineering Properties Common Composite Laminate Tape

Engineering Materials

Wet Laminate Carbon Tape engineering properties in both SI and imperial units.

Wet Laminate Carbon Tape Engineering Data SI Units

Description
Hot Wet
Hot
RT
Cold
Minimum
(160F, 95% RH)
(160F)
(75F)
(-65F)
-
Ftu 1 (Mpa)
1801.8
1886.4
2008.8
1970.1
1801.8
E t11 (Mpa)
110000.0
110000.0
110000.0
110000.0
110000.0
Ftu 2 (Mpa)
11.7
24.3
28.8
30.6
11.7
E t22 (Mpa)
6325.3
6325.3
6325.3
6325.3
6325.3
v 12 (Mpa)
0.314
0.314
0.314
0.314
0.314
Fcu 1 (Mpa)
558.9
926.1
932.4
1068.3
558.9
E c11 (Mpa)
110000.0
110000.0
110000.0
110000.0
110000.0
Fcu 2 (Mpa)
67.5
118.8
145.8
198.9
67.5
E c22 (Mpa)
7101.6
7101.6
7101.6
7101.6
7101.6
Fsu 12 (Mpa)
56.7
83.7
106.2
132.3
56.7
G 12 (Mpa)
2620.0
2620.0
2620.0
2620.0
2620.0
ILS
0.0
0.0
0.0
0.0
0.0
Thickness (mm)*
0.43
0.43
0.43
0.43
-
E av11 (Mpa)
110000.0
110000.0
110000.0
110000.0
110000.0
E av22 (Mpa)
6713.5
6713.5
6713.5
6713.5
6713.5
CAI Compression Strain
3000.0
4971.0
5004.8
5734.3
3000.0
Filled Hole Tension Strain
4500.0
4711.3
5017.0
4920.3
4500.0
Open Hole Tension Stress (Mpa)
-
-
-
-
-
Open Hole Compression Stress (Mpa)
160.5
-
263.5
-
160.5
Filled Hole Tensions Stress (Mpa)
-
-
445.1
-
445.1
Filled Hole Compression Stress (Mpa)
275.6
-
 
-
275.6
50% Bypass Tension Stress (Mpa)
-
-
685.0
-
685.0
50% Bypass Compression Stress (Mpa)
-
-
694.2
-
694.2
25% Bypass Tension Stress (Mpa)
-
-
1276.2
-
1276.2
25% Bypass Compression Stress (Mpa)
-
-
1205.6
-
1205.6
Single Shear Bearing Stress (Mpa)
536.4
-
666.0
-
536.4
Double Shear Bearing (Mpa)
257.0
-
448.7
-
257.0

* Check Thickness Values against specific project material


Wet Laminate Carbon Tape Engineering Data Imperial Units

Description
Hot Wet
Hot
RT
Cold
Minimum
(160F, 95% RH)
(160F)
(75F)
(-65F)
-
F tu1 (psi)
261329
273599
291352
285739
261329
E t11 (psi)
15954151
15954151
15954151
15954151
15954151
F tu2 (psi)
1697
3524
4177
4438
1697
E t22 (psi)
917407
917407
917407
917407
917407
v 12
0.31
0.31
0.31
0.31
0.31
F cu1 (psi)
81062
134319
135233
154944
81062
E c11 (psi)
15954151
15954151
15954151
15954151
15954151
F cu2 (psi)
9790
17230
21147
28848
9790
E c22 (psi)
1030000
1030000
1030000
1030000
1030000
F su12 (psi)
8224
12140
15403
19188
8224
G 12 (psi)
379999
379999
379999
379999
379999
ILS
-
-
0
0
0
Thickness (in)*
0.0169
0.0169
0.0169
0.0169
-
E av11 (psi)
15954151
15954151
15954151
15954151
15954151
E av22 (psi)
973704
973704
973704
973704
973704
CAI Compression Strain
3000.0
4971.0
5004.8
5734.3
3000.0
Filled Hole Tension Strain
4500.0
4711.3
5017.0
4920.3
4500.0
Open Hole Tension Stress (psi)
-
-
-
-
-
Open Hole Compression Stress (psi)
23274
-
38220
-
23274
Filled Hole Tensions Stress (psi)
-
-
64549
-
64549
Filled Hole Compression Stress (psi)
39969
-
-
-
39969
50% Bypass Tension Stress (psi)
-
-
99349
-
99349
50% Bypass Compression Stress (psi)
-
-
100681
-
100681
25% Bypass Tension Stress (psi)
-
-
185097
-
185097
25% Bypass Compression Stress (psi)
-
-
174863
-
174863
Single Shear Bearing Stress (psi)
77798
-
96595
-
77798
Double Shear Bearing (psi)
37281
-
65071
-
37281

* Check Thickness Values against specific project material

Contribute Article
Spider Optimizer

© Copyright 2000 - 2017, by Engineers Edge, LLC www.engineersedge.com
All rights reserved
Disclaimer | Feedback | Advertising | Contact


User Reviews/Comments:

There are currently no comments available.


Add a Comment (you must be logged in to post comment Register):
Name:
Email: (Optional)
Comment: