Experimental Validation of Polynomial Chaos Theory on an Aircraft T-Tail
Author:
Affiliation:
1. University of Sydney
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0953
Reference39 articles.
1. Uncertainty Quantification in Aeroelasticity: Recent Results and Research Challenges
2. The Monte Carlo method in science and engineering
3. Monte Carlo studies of engineering system reliability
4. Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures
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