Re-use of this resource is governed by a Creative Commons Attribution-
Noncommercial-Share Alike 2.0 Licence UK: England & Wales
https://creativecommons.org/licenses/by-nc-sa/2.0/uk/
creative commons DoITPoMS logo
Φ Max 300 Min -3 0 0 10 20 30 40 50 60 70 80 90 Φ y x
Matrices
Epoxy
Polyester
Nylon6,6
PEEK
Al

Fibres
SiC
CarbonHM
CarbonHS
E glass
Kevlar49

Ply  θ  Constituents    f%
1
Epoxy
SiC
2
Epoxy
SiC

3
Epoxy
SiC

4
Epoxy
SiC

5
Epoxy
SiC
Construct your own laminate by dragging the fibres
and number of plies (k), fibre orientations (θ) and fibre
volume fractions (f) before calculating tensile-shear
interactions for different loading angles.

Please insert angles
between -90 and 90 only.