Related Resources: materials
Engineering Properties Common Composite Laminate Tape
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