Response surface approximations for cost optimization of dropped ply composite laminates with uncertainty-Reference-Cited by-同舟云学术

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Response surface approximations for cost optimization of dropped ply composite laminates with uncertainty

Published:1998-08-22 Issue: Volume: Page:
ISSN:
Container-title:7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
language:
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Author:

Venter Gerhard¹,Haftka Raphael¹

Affiliation:

1. Florida, Univ., Gainesville

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-4856

Reference29 articles.

1. Response and failure analysis of a graphite-epoxy laminate containing terminating internal plies

2. Tensile strength of tapered composite structures

3. Effect of dropped plies on the strength of graphite-epoxy laminates

4. The Effect of Film Adhesive on the Delamination Strength of Tapered Composites

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Material Uncertainty Propagation in Helicopter Nonlinear Aeroelastic Response and Vibratory Analysis;AIAA Journal;2008-09

2. Response Surface Approximations: Noise, Error Repair, and Modeling Errors;AIAA Journal;2000-12

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