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Design optimization of hot-air anti-icing systems by FENSAP-ICE

  • Published:2010-01-04 Issue: Volume: Page:
  • ISSN:
  • Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
  • language:
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Author:

Pellissier Mathieu1,Habashi Wagdi1,Pueyo Alberto1

Affiliation:

1. McGill University

Publisher

American Institute of Aeronautics and Astronautics

Reference52 articles.

1. 1NationalTransportationSafetyBoard,"AnnualReviewofAircraftAccidentData",U.S.GeneralAviation,2005.

2. Aircraft icing environments observed in mixed-phase clouds

3. 5"AirworthinessStandards:TransportCategoryAirplanes,Part25,AppendixC",FederalAviationAdministration,2007.

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1. Effects of Film Holes Position on Anti-icing Characteristics of Aero-engine Inlet Adjustable Blade;Lecture Notes in Mechanical Engineering;2023-12-20

2. Thermal Feature Analysis of a New Hot-Air Anti-Icing Structure;Journal of Thermal Science;2023-02-20

3. Experimental investigation on de-icing by an array of impact rod-type plasma synthetic jets;Plasma Science and Technology;2023-01-18

4. On a reduced-order model-based optimization of rotor electro-thermal anti-icing systems;International Journal of Numerical Methods for Heat & Fluid Flow;2022-01-10

5. Parametric Investigation of High-voltage Plasma Discharge for Aircraft Icing Mitigation;2021 IEEE 2nd China International Youth Conference on Electrical Engineering (CIYCEE);2021-12-15
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