1. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Framework for a Combined Netting Analysis and Tsai-Wu-Based Design Approach for Braided and Filament-Wound Composites
J. Pressure Vessel Technol. 2013;135(3): doi: /
Figure Legend:
General mandrel shape

2. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Framework for a Combined Netting Analysis and Tsai-Wu-Based Design Approach for Braided and Filament-Wound Composites
J. Pressure Vessel Technol. 2013;135(3): doi: /
Figure Legend:
Variation of failure index f with fiber angle α in glass/epoxy for a constant stress ratio k and different axial stresses (MPa), with failure line at f = 1

3. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Framework for a Combined Netting Analysis and Tsai-Wu-Based Design Approach for Braided and Filament-Wound Composites
J. Pressure Vessel Technol. 2013;135(3): doi: /
Figure Legend:
Variation of failure index f with fiber angle α in carbon/epoxy for a constant stress ratio k and different axial stresses, with failure line at f = 1

4. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Framework for a Combined Netting Analysis and Tsai-Wu-Based Design Approach for Braided and Filament-Wound Composites
J. Pressure Vessel Technol. 2013;135(3): doi: /
Figure Legend:
Variation of failure index f with fiber angle α in glass/epoxy for a constant axial stress a and different stress ratios k, with failure line at f = 1

5. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Framework for a Combined Netting Analysis and Tsai-Wu-Based Design Approach for Braided and Filament-Wound Composites
J. Pressure Vessel Technol. 2013;135(3): doi: /
Figure Legend:
Variation of failure index f with fiber angle α in carbon/epoxy for a constant axial stress a and different stress ratios k, with failure line at f = 1

6. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Framework for a Combined Netting Analysis and Tsai-Wu-Based Design Approach for Braided and Filament-Wound Composites
J. Pressure Vessel Technol. 2013;135(3): doi: /
Figure Legend:
Variation of critical fiber angle αcritical with axial stress a in glass/epoxy and carbon/epoxy for a constant stress ratio k = 1.96

7. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Framework for a Combined Netting Analysis and Tsai-Wu-Based Design Approach for Braided and Filament-Wound Composites
J. Pressure Vessel Technol. 2013;135(3): doi: /
Figure Legend:
Variation of critical fiber angle αcritical with hoop-to-axial stress ratio k in glass/epoxy and carbon/epoxy for an axial stress a = 20 MPa

8. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Framework for a Combined Netting Analysis and Tsai-Wu-Based Design Approach for Braided and Filament-Wound Composites
J. Pressure Vessel Technol. 2013;135(3): doi: /
Figure Legend:
Variation of αcritical with stress ratio k in (a) glass/epoxy and (b) carbon/epoxy for constant axial stresses of a = 10, 20, and 30 MPa

9. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Framework for a Combined Netting Analysis and Tsai-Wu-Based Design Approach for Braided and Filament-Wound Composites
J. Pressure Vessel Technol. 2013;135(3): doi: /
Figure Legend:
Variation of αcritical with axial stress a in glass/epoxy for constant hoop-to-axial stress ratios k = 1.96, 4, and 10

10. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Framework for a Combined Netting Analysis and Tsai-Wu-Based Design Approach for Braided and Filament-Wound Composites
J. Pressure Vessel Technol. 2013;135(3): doi: /
Figure Legend:
Variation of αcritical with axial stress a in glass/epoxy for pure axial loading (k = 0)

11. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Framework for a Combined Netting Analysis and Tsai-Wu-Based Design Approach for Braided and Filament-Wound Composites
J. Pressure Vessel Technol. 2013;135(3): doi: /
Figure Legend:
Comparison of αcritical from present analysis with results by Srikanth and Rao [12] for pure axial loading (k = 0)