1. From: Constitutive Model for Fiber-Reinforced Composite Laminates
Date of download: 12/24/2017
Copyright © ASME. All rights reserved.
From: Constitutive Model for Fiber-Reinforced Composite Laminates
J. Appl. Mech. 2006;73(6): doi: /
Figure Legend:
Numerical scheme for the solution of a nonlinear problem

2. From: Constitutive Model for Fiber-Reinforced Composite Laminates
Date of download: 12/24/2017
Copyright © ASME. All rights reserved.
From: Constitutive Model for Fiber-Reinforced Composite Laminates
J. Appl. Mech. 2006;73(6): doi: /
Figure Legend:
Fiber reinforced laminated composite

3. From: Constitutive Model for Fiber-Reinforced Composite Laminates
Date of download: 12/24/2017
Copyright © ASME. All rights reserved.
From: Constitutive Model for Fiber-Reinforced Composite Laminates
J. Appl. Mech. 2006;73(6): doi: /
Figure Legend:
Failure envelope for a unidirectional lamina (E-Glass/LY556/HT907/DY063)

4. From: Constitutive Model for Fiber-Reinforced Composite Laminates
Date of download: 12/24/2017
Copyright © ASME. All rights reserved.
From: Constitutive Model for Fiber-Reinforced Composite Laminates
J. Appl. Mech. 2006;73(6): doi: /
Figure Legend:
Failure envelope for a unidirectional lamina (T300/BSL914C epoxy)

5. From: Constitutive Model for Fiber-Reinforced Composite Laminates
Date of download: 12/24/2017
Copyright © ASME. All rights reserved.
From: Constitutive Model for Fiber-Reinforced Composite Laminates
J. Appl. Mech. 2006;73(6): doi: /
Figure Legend:
Failure envelope for a unidirectional lamina (Silenka E-Glass 1200 tex MY750/HY917/DY063 epoxy)

6. From: Constitutive Model for Fiber-Reinforced Composite Laminates
Date of download: 12/24/2017
Copyright © ASME. All rights reserved.
From: Constitutive Model for Fiber-Reinforced Composite Laminates
J. Appl. Mech. 2006;73(6): doi: /
Figure Legend:
Failure envelope for (90deg∕±45deg∕0deg)s laminate (AS4/3501-6)

7. From: Constitutive Model for Fiber-Reinforced Composite Laminates
Date of download: 12/24/2017
Copyright © ASME. All rights reserved.
From: Constitutive Model for Fiber-Reinforced Composite Laminates
J. Appl. Mech. 2006;73(6): doi: /
Figure Legend:
Failure envelope for (±55deg)s laminate (Silenka E-Glass 1200 tex MY750/HY917/DY063 epoxy)