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1
Monitoring Impact Events Using a System-Identification Method
Monitoring Impact Events Using a System-Identification Method
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Monitoring Impact Events Using a System-Identification Method

Park, Jonghyun ; Ha, Sungwon ; Chang, Fu-Kuo

AIAA journal, 2009-09, Vol.47 (9), p.2011-2021 [Periódico revisado por pares]

Reston, VA: American Institute of Aeronautics and Astronautics

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2
Modeling and Dynamics of Sandwich Beams with a Viscoelastic Soft Core
Modeling and Dynamics of Sandwich Beams with a Viscoelastic Soft Core
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Modeling and Dynamics of Sandwich Beams with a Viscoelastic Soft Core

Hamed, Ehab ; Rabinovitch, Oded

AIAA journal, 2009-09, Vol.47 (9), p.2194-2211 [Periódico revisado por pares]

Reston, VA: American Institute of Aeronautics and Astronautics

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3
Consistent Higher-Order Dynamic Equations for Soft-Core Sandwich Beams
Consistent Higher-Order Dynamic Equations for Soft-Core Sandwich Beams
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Consistent Higher-Order Dynamic Equations for Soft-Core Sandwich Beams

Sokolinsky, Vladimir S ; Nutt, Steven R

AIAA journal, 2004-02, Vol.42 (2), p.374-382 [Periódico revisado por pares]

Reston, VA: American Institute of Aeronautics and Astronautics

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4
Multiple-Timescale Analysis for Bifurcation from a Multiple-Zero Eigenvalue
Multiple-Timescale Analysis for Bifurcation from a Multiple-Zero Eigenvalue
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Multiple-Timescale Analysis for Bifurcation from a Multiple-Zero Eigenvalue

Luongo, Angelo ; Di Egidio, Angelo ; Paolone, Achille

AIAA journal, 2003-06, Vol.41 (6), p.1143-1150 [Periódico revisado por pares]

Reston, VA: American Institute of Aeronautics and Astronautics

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5
Electromechanically Coupled Zigzag Third-Order Theory for Thermally Loaded Hybrid Piezoelectric Plates
Electromechanically Coupled Zigzag Third-Order Theory for Thermally Loaded Hybrid Piezoelectric Plates
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Electromechanically Coupled Zigzag Third-Order Theory for Thermally Loaded Hybrid Piezoelectric Plates

Kapuria, S ; Achary, G. G. S

AIAA journal, 2006-01, Vol.44 (1), p.160-170 [Periódico revisado por pares]

Reston, VA: American Institute of Aeronautics and Astronautics

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6
Efficient Coupled Zigzag Theory for Hybrid Piezoelectric Beams for Thermoelectric Load
Efficient Coupled Zigzag Theory for Hybrid Piezoelectric Beams for Thermoelectric Load
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Efficient Coupled Zigzag Theory for Hybrid Piezoelectric Beams for Thermoelectric Load

Kapuria, S ; Dumir, P. C ; Ahmed, A

AIAA journal, 2004-02, Vol.42 (2), p.383-394 [Periódico revisado por pares]

Reston, VA: American Institute of Aeronautics and Astronautics

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7
Buckling and Vibration Analysis of Composite Sandwich Plates with Elastic Rotational Edge Restraints
Buckling and Vibration Analysis of Composite Sandwich Plates with Elastic Rotational Edge Restraints
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Buckling and Vibration Analysis of Composite Sandwich Plates with Elastic Rotational Edge Restraints

Rais-Rohani, Masoud ; Marcellier, Pierre

AIAA journal, 1999-05, Vol.37 (5), p.579-587 [Periódico revisado por pares]

Virginia: American Institute of Aeronautics and Astronautics

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8
Boundary Condition Effects in Free Vibrations of Higher-Order Soft Sandwich Beams
Boundary Condition Effects in Free Vibrations of Higher-Order Soft Sandwich Beams
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Boundary Condition Effects in Free Vibrations of Higher-Order Soft Sandwich Beams

Sokolinsky, Vladimir S ; Nutt, Steven R ; Frostig, Yeoshua

AIAA journal, 2002-06, Vol.40 (6), p.1220-1227 [Periódico revisado por pares]

Reston, VA: American Institute of Aeronautics and Astronautics

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9
High-Order Analysis of Unidirectional Sandwich Panels with Piezolaminated Face Sheets and Soft Core
High-Order Analysis of Unidirectional Sandwich Panels with Piezolaminated Face Sheets and Soft Core
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High-Order Analysis of Unidirectional Sandwich Panels with Piezolaminated Face Sheets and Soft Core

Rabinovitch, Oded ; Vinson, Jack R ; Frostig, Yeoshua

AIAA journal, 2003-01, Vol.41 (1), p.110-118 [Periódico revisado por pares]

Reston, VA: American Institute of Aeronautics and Astronautics

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10
Dynamic Response of Adaptive Cross-Ply Cantilevers Featuring Interlaminar Bonding Imperfections
Dynamic Response of Adaptive Cross-Ply Cantilevers Featuring Interlaminar Bonding Imperfections
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Dynamic Response of Adaptive Cross-Ply Cantilevers Featuring Interlaminar Bonding Imperfections

Icardi, U ; Di Sciuva, M ; Librescu, L

AIAA journal, 2000-03, Vol.38 (3), p.499-506 [Periódico revisado por pares]

Reston, VA: American Institute of Aeronautics and Astronautics

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