Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Analysis range and coordinate system of the stiffened panels. (a) Mode A: 1/2 + 1 + 1/2 spans, (b) Model B: 1 + 1 spans, and (c) Model C: 1/2 + 1 + 1 + 1/2 spans.

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Engineering and true stress-strain curves of the material

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: FE models of the stiffened panels. (a) Mode A: 1/2 + 1 + 1/2 spans, (b) Model B: 1 + 1 spans, and (c) Model C: 1/2 + 1 + 1 + 1/2 spans.

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Initial imperfection shapes of the stiffened panel for Model A. (a) Local plate panel, (b) Column-type of stiffeners, and (c) Side-ways of stiffeners.

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Failure mode and equivalent stress distributions of the stiffened panels at ultimate strength under longitudinal thrust (L = 300 mm, tp = 4 mm). (a) Case 1, (b) Case 2, (c) Case 3, and (d) Case 4.

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Ultimate strength of the stiffened panels under longitudinal thrust (tp = 4 mm)

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Load-displacement curves of the stiffened panels under pure longitudinal thrust (tp = 4 mm). (a) L = 300 mm, (b) L = 450 mm, (c) L = 600 mm.

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Equivalent stress distributions of the stiffened panels after collapse under pure longitudinal thrust (L = 300 mm, tp = 4 mm). (a) Case 1, (b) Case 2, (c) Case 3, and (d) Case 4.

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Relationships between the ultimate strength and plate panel slenderness of the stiffened panels under pure longitudinal thrust. (a) L = 300 mm, (b) L = 450 mm, and (c) L = 600 mm.

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Load-displacement curves of the stiffened panels under combined longitudinal thrust and lateral pressure (L = 450 mm, tp = 4 mm). (a) Lateral pressure: 0.2 MPa and (b) Lateral pressure: 0.4 MPa.

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Ultimate strength of the stiffened panels under combined longitudinal thrust and lateral pressure (L = 450 mm, tp = 4 mm). (a) Lateral pressure: 0.2 MPa and (b) Lateral pressure: 0.4 MPa.

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Failure mode and equivalent stress distributions of the stiffened panels at the ultimate strength under the combined load (FS45B2, L = 450 mm, lateral pressure = 0.4 MPa). (a) Case 1, (b) Case 2, (c) Case 3, and (d) Case 4.

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Ultimate strength of the stiffened panels with different lateral pressure (L = 450 mm, Case 2)

Date of download: 11/13/2017 Copyright © ASME. All rights reserved. From: Influence of Model Geometry and Boundary Conditions on the Ultimate Strength of Stiffened Panels Under Uniaxial Compressive Loading J. Offshore Mech. Arct. Eng. 2013;135(4):041603-041603-10. doi:10.1115/1.4024710 Figure Legend: Collapse modes of the stiffened panels at the ultimate strength with different lateral pressures for FS45B2 (L = 450 mm, Case 2). (a) Lateral pressure = 0, (b) Lateral pressure = 0.1 MPa, (c) Lateral pressure = 0.2 MPa, (d) Lateral pressure = 0.3 MPa, and (e) Lateral pressure = 0.4 MPa.