Uncertainty Quantification for Airfoil Icing Using Polynomial Chaos Expansions
Author:
Affiliation:
1. Mechanical and Aerospace Engineering, Princeton University, Princeton, New Jersey 08540
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032698
Reference17 articles.
1. WrightW. “User’s Manual for LEWICE Version 3.2,” NASA/Contractor's Rept. 214255, 2008.
2. Extension to the Messinger Model for Aircraft Icing
3. Iced-airfoil aerodynamics
4. A study of large droplet ice accretions in the NASA-Lewis IRT at near-freezing conditions
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