Surrogate-Based Optimization of Electrothermal Wing Anti-Icing Systems
Author:
Affiliation:
1. CFD Laboratory, Department of Mechanical Engineering, McGill University, Montreal, Quebec H3A 2S6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032072
Reference23 articles.
1. Aircraft anti-icing and de-icing techniques and modeling
2. Water Droplet Impact Dynamics at Icing Conditions with and without Superhydrophobicity
3. Advanced pneumatic impulse ice protection system (PIIP) for aircraft
4. ZumwaltG.SchragR.BernhartW.FriedbergR. “Electro-Impulse De-Icing Testing Analysis and Design,” NASA Contractor, Rept. 4175, 1988.
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