Fatigue Crack Growth Predictions in Aging Aircraft Panels Using Optimization Neural Network
Author:
Affiliation:
1. Purdue University at Indianapolis, Indianapolis,Indiana 46202
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.514
Reference22 articles.
1. Influence of fastener holes on residual strength
2. Structural Integrity of Aging Airplanes
3. Analysis of cracks in aging aircraft structures, with and without composite-patch repairs
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