1. Date of download: 12/23/2017
Copyright © ASME. All rights reserved.
From: Superharmonic Resonance of Cross-Ply Laminates by the Method of Multiple Scales
J. Comput. Nonlinear Dynam. 2017;12(5): doi: /
Figure Legend:
Laminated composite beam geometry under uniform distributed load q(t)

2. Date of download: 12/23/2017
Copyright © ASME. All rights reserved.
From: Superharmonic Resonance of Cross-Ply Laminates by the Method of Multiple Scales
J. Comput. Nonlinear Dynam. 2017;12(5): doi: /
Figure Legend:
Nonlinear amplitude frequency responses of the stacking sequence (−45 deg/45 deg/−45 deg/45 deg/−45 deg/45 deg/−45 deg/45 deg) composite beam when ω is near ωl/3, according to different kinematical models

3. Date of download: 12/23/2017
Copyright © ASME. All rights reserved.
From: Superharmonic Resonance of Cross-Ply Laminates by the Method of Multiple Scales
J. Comput. Nonlinear Dynam. 2017;12(5): doi: /
Figure Legend:
Nonlinear amplitude frequency responses with Reddy model when ω is near ωl/3 according to the different stacking sequences of the composite beams

4. Date of download: 12/23/2017
Copyright © ASME. All rights reserved.
From: Superharmonic Resonance of Cross-Ply Laminates by the Method of Multiple Scales
J. Comput. Nonlinear Dynam. 2017;12(5): doi: /
Figure Legend:
Nonlinear amplitude frequency responses of the stacking sequence (−45 deg/45 deg/−45 deg/45 deg/−45 deg/45 deg/−45 deg/45 deg) composite beam with Reddy model when ω is near ωl/3 for different amplitude of excitation F

5. Date of download: 12/23/2017
Copyright © ASME. All rights reserved.
From: Superharmonic Resonance of Cross-Ply Laminates by the Method of Multiple Scales
J. Comput. Nonlinear Dynam. 2017;12(5): doi: /
Figure Legend:
Nonlinear amplitude frequency responses of the stacking sequence (−45 deg/45 deg/−45 deg/45 deg/−45 deg/45 deg/−45 deg/45 deg) composite beam with Reddy model when ω is near ωl/3 for different values of loss factor η1