On Composite Laminates with Extensional-Anisotropy-Reference-Cited by-同舟云学术

On Composite Laminates with Extensional-Anisotropy

Published:2008-04-07 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 16th AIAA/ASME/AHS Adaptive Structures Conference 10t
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Author:

York Christopher

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. Response of Damaged and Undamaged Tailored Extension-Shear-Coupled Composite Panels

2. 5York, C. B. "Characterizationand Ply Mixing Rules for Non-symmetric Forms of Fully OrthotropicLaminates,"Proc. 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf., Paper No. AIAA-2007-2083.Honolulu, Hawaii, 2007.

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2. Unified approach to the characterization of coupled composite laminates;International Journal of Structural Integrity;2011-11-22

3. Unified Approach to the Characterization of Coupled Composite Laminates: Benchmark Configurations and Special Cases;Journal of Aerospace Engineering;2010-10

4. Approximations for Warp-Free Laminate Configurations;51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference 12th;2010-04-12

5. Stacking Sequences for Extensionally Isotropic, Fully Isotropic and Quasi-Homogeneous Orthotropic Laminates;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 16th AIAA/ASME/AHS Adaptive Structures Conference 10t;2008-04-07