Related Resources: materials
Engineering Properties Common Composite Laminates
Wet Laminate Carbon Cloth engineering properties in both SI and imperial units.
Wet Laminate Carbon Cloth Engineering Data SI Units
Description |
Hot Wet |
Hot |
RT |
Cold |
Minimum |
(160F, 95% RH) |
(160F) |
(75F) |
(-65F) |
- |
|
Ftu 1 (Mpa) |
622.0 |
676.0 |
725.0 |
762.0 |
622.0 |
E t11 (Mpa) |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
Ftu 2 (Mpa) |
527.0 |
671.0 |
684.0 |
722.0 |
527.0 |
E t22 (Mpa) |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
v 12 (Mpa) |
0.030 |
0.030 |
0.030 |
0.030 |
0.030 |
Fcu 1 (Mpa) |
378.0 |
451.0 |
518.0 |
520.0 |
378.0 |
E c11 (Mpa) |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
Fcu 2 (Mpa) |
350.0 |
418.0 |
480.0 |
480.0 |
350.0 |
E c22 (Mpa) |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
Fsu 12 (Mpa) |
49.0 |
58.0 |
67.0 |
79.0 |
49.0 |
G 12 (Mpa) |
2700.0 |
2700.0 |
2700.0 |
2700.0 |
2700.0 |
ILS |
- |
- |
38.0 |
47.0 |
38.0 |
Thickness (mm)* |
0.24 |
0.24 |
0.24 |
0.24 |
- |
E av11 (Mpa) |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
E av22 (Mpa) |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
60000.0 |
CAI Compression Strain |
3000.0 |
3579.4 |
4111.1 |
4127.0 |
3000.0 |
Filled Hole Tension Strain |
4500.0 |
4890.7 |
5245.2 |
5512.9 |
4500.0 |
Open Hole Tension Stress (Mpa) |
- |
- |
- |
- |
- |
Open Hole Compression Stress (Mpa) |
147.1 |
- |
246.2 |
- |
147.1 |
Filled Hole Tensions Stress (Mpa) |
- |
- |
262.1 |
- |
262.1 |
Filled Hole Compression Stress (Mpa) |
229.3 |
- |
- |
229.3 |
|
50% Bypass Tension Stress (Mpa) |
- |
- |
622.4 |
- |
622.4 |
50% Bypass Compression Stress (Mpa) |
- |
- |
637.5 |
- |
637.5 |
25% Bypass Tension Stress (Mpa) |
- |
- |
737.4 |
- |
737.4 |
25% Bypass Compression Stress (Mpa) |
- |
- |
1160.0 |
- |
1160.0 |
Single Shear Bearing Stress (Mpa) |
504.8 |
- |
660.1 |
- |
504.8 |
Double Shear Bearing (Mpa) |
278.6 |
- |
480.4 |
- |
278.6 |
* Check Thickness Values against specific project material
Wet Laminate Carbon Cloth Engineering Data Imperial Units
Description |
Hot Wet |
Hot |
RT |
Cold |
Minimum |
(160F, 95% RH) |
(160F) |
(75F) |
(-65F) |
- |
|
F tu1 (psi) |
8702264 |
8702264 |
8702264 |
8702264 |
8702264 |
E t11 (psi) |
435113 |
519143 |
596266 |
598568 |
435113 |
F tu2 (psi) |
652670 |
709332 |
760749 |
799573 |
652670 |
E t22 (psi) |
0 |
0 |
0 |
0 |
0 |
v 12 |
0.030 |
0.030 |
0.030 |
0.030 |
0 |
F cu1 (psi) |
0 |
0 |
38011 |
0 |
0 |
E c11 (psi) |
33260 |
0 |
0 |
0 |
0 |
F cu2 (psi) |
0 |
0 |
90277 |
0 |
0 |
E c22 (psi) |
0 |
0 |
92457 |
0 |
0 |
F su12 (psi) |
0 |
0 |
106946 |
0 |
0 |
G 12 (psi) |
0 |
0 |
168245 |
0 |
0 |
ILS |
- |
- |
95734 |
0 |
0 |
Thickness (in)* |
10.9701 |
0.0000 |
18.9142 |
0.0000 |
- |
E av11 (psi) |
0 |
0 |
0 |
0 |
0 |
E av22 (psi) |
0 |
0 |
0 |
0 |
0 |
CAI Compression Strain |
0.0 |
0.0 |
- |
0.0 |
0 |
Filled Hole Tension Strain |
0.0 |
0.0 |
- |
0.0 |
0 |
Open Hole Tension Stress (psi) |
- |
- |
- |
- |
- |
Open Hole Compression Stress (psi) |
0 |
- |
- |
- |
- |
Filled Hole Tensions Stress (psi) |
- |
- |
- |
- |
- |
Filled Hole Compression Stress (psi) |
0 |
- |
- |
- |
0 |
50% Bypass Tension Stress (psi) |
- |
- |
0 |
- |
0 |
50% Bypass Compression Stress (psi) |
- |
- |
0 |
- |
0 |
25% Bypass Tension Stress (psi) |
- |
- |
0 |
- |
0 |
25% Bypass Compression Stress (psi) |
- |
- |
0 |
- |
0 |
Single Shear Bearing Stress (psi) |
0 |
- |
0 |
- |
0 |