Numerical and Experimental Investigation of the Design of a Piezoelectric De-Icing System for Small Rotorcraft Part 1/3: Development of a Flat Plate Numerical Model with Experimental Validation

The objective of this research project is divided in four parts: (1) to design a piezoelectric actuator-based de-icing system integrated to a flat plate experimental setup and develop a numerical model of the system with experimental validation, (2) use the experimental setup to investigate actuator...

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Bibliographic Details
Main Authors: Eric Villeneuve, Christophe Volat, Sebastian Ghinet
Format: Article
Language:English
Published: MDPI AG 2020-05-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/7/5/62