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Higher-Order Buckling of Debonded (Delaminated) Sandwich Panels with Soft Core
Higher-Order Buckling of Debonded (Delaminated) Sandwich Panels with Soft Core
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Higher-Order Buckling of Debonded (Delaminated) Sandwich Panels with Soft Core

Frostig, Y ; Sokolinsky, V

AIAA journal, 2000-11, Vol.38 (11), p.2147-2159 [Periódico revisado por pares]

Reston, VA: American Institute of Aeronautics and Astronautics

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2
Natural Frequencies of Cross-Ply Laminated Panels with Matrix Cracks
Natural Frequencies of Cross-Ply Laminated Panels with Matrix Cracks
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Natural Frequencies of Cross-Ply Laminated Panels with Matrix Cracks

Birman, Victor ; Byrd, Larry W

AIAA journal, 2001-01, Vol.39 (1), p.190-193 [Periódico revisado por pares]

Reston, VA: American Institute of Aeronautics and Astronautics

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3
Failure of tapered composites under static and fatigue tension loading
Failure of tapered composites under static and fatigue tension loading
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Failure of tapered composites under static and fatigue tension loading

Wisnom, Michael R ; Jones, M I ; Cui, Weicheng

AIAA Journal, 1995-05, Vol.33 (5), p.911-918 [Periódico revisado por pares]

Virginia: American Institute of Aeronautics and Astronautics

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4
Optimal through-thickness temperature gradients for control of interlaminar stresses in composites
Optimal through-thickness temperature gradients for control of interlaminar stresses in composites
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Optimal through-thickness temperature gradients for control of interlaminar stresses in composites

Kim, Taehyoun ; Atluri, Satya N

AIAA journal, 1995-04, Vol.33 (4), p.730-738 [Periódico revisado por pares]

Virginia: American Institute of Aeronautics and Astronautics

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