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![Preliminary 3D printed nacre-like composite prototypes of different shapes and material combinations.](thumbnails/s256.jpg) |
![Multiscale simulation strategy in connection with composite materials used for aircraft](thumbnails/s257.jpg) |
![Elastic beam subjected to time-varying lateral distributed load q](thumbnails/s258.jpg) |
![Non-chaotic behavior of the beam for a low-amplitude load, q-sub-0 = 200](thumbnails/s259.jpg) |
![Partially chaotic behavior of the beam at the load amplitude, q-sub-0 = 1000](thumbnails/s260.jpg) |
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Preliminary 3D printed nacre-like composite prototypes of different shapes and material combinations. |
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Multiscale simulation strategy in connection with composite materials used for aircraft |
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Elastic beam subjected to time-varying lateral distributed load q |
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Non-chaotic behavior of the beam for a low-amplitude load, q-sub-0 = 200 |
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Partially chaotic behavior of the beam at the load amplitude, q-sub-0 = 1000 |
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![More chaotic behavior of the beam at the load amplitude, q-sub-0 = 39000](thumbnails/s261.jpg) |
![Axially compressed nonlinear dynamic behavior of a plate for two normalized loads Po = 4 and Po =8.25](thumbnails/s262.jpg) |
![Nonlinear dynamic response of a locally transversely loaded shallow shell for 4 pairs (qo,omegap) of load amplitude qo and frequency omegap](thumbnails/s263.jpg) |
![Chaotic dynamic response of cylindrical shell with a transverse patch load, q = qosin(omegayt)](thumbnails/s264.jpg) |
![Shell vibration regimes including chaos](thumbnails/s265.jpg) |
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More chaotic behavior of the beam at the load amplitude, q-sub-0 = 39000 |
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Axially compressed nonlinear dynamic behavior of a plate for two normalized loads Po = 4 and Po =8.25 |
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Nonlinear dynamic response of a locally transversely loaded shallow shell for 4 pairs (qo,omegap) of load amplitude qo and frequency omegap |
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Chaotic dynamic response of cylindrical shell with a transverse patch load, q = qosin(omegayt) |
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Shell vibration regimes including chaos |
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![Plan views of paired buckling modes of any closed isotropic shell of revolution](thumbnails/s266.jpg) |
![Substructuring of an airplane wing](thumbnails/s267.jpg) |
![Undeformed and deformed attice with (a) tension and (b) compression applied in the horizontal direction](thumbnails/s268.jpg) |
![Buckling and large deflection of thin band](thumbnails/s269.jpg) |
![Beam with actuator (bottom) and sensor (top) piezoelectric patches for controlling and sensing free vibration from a suddenly removed load at the tip](thumbnails/s270.jpg) |
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Plan views of paired buckling modes of any closed isotropic shell of revolution |
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Substructuring of an airplane wing |
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Undeformed and deformed attice with (a) tension and (b) compression applied in the horizontal direction |
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Buckling and large deflection of thin band |
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Beam with actuator (bottom) and sensor (top) piezoelectric patches for controlling and sensing free vibration from a suddenly removed load at the tip |
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