An approach to the design of aircraft structures with damage tolerance requirements-Reference-Cited by-同舟云学术

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An approach to the design of aircraft structures with damage tolerance requirements

Published:2000-04-03 Issue: Volume: Page:
ISSN:
Container-title:41st Structures, Structural Dynamics, and Materials Conference and Exhibit
language:
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Author:

Arrieta Albert¹,Striz Alfred¹,Venkayya Vipperla²

Affiliation:

1. Oklahoma, Univ., Norman

2. USAF, Research Lab., Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-1786

Reference11 articles.

1. The Practical Use of Fracture Mechanics

2. Chaperon, P., Sawyer, J. P.,and Jones, R. "Efficient Computational Methodology For Damage Tolerance Assessments In Conjunction With Structural Optimisation: Phase II, Interim Report". Monc 1sh University, COE-SM 97-P04, Victoria. Australia. i\pril 1999.

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. Tradeoff of Structural Weight and Inspection Cost in Reliability Based Optimization Using Multiple Inspection Types;10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2004-08-30

2. Tradeoffs of Weight and Inspection Cost in Fail-safe Design;44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2003-04-07

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