Código QR

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...

Descrición completa

Gardado en:
Detalles Bibliográficos
Principais autores: Eric Villeneuve, Christophe Volat, Sebastian Ghinet
Formato: Artigo
Idioma:Inglês
Publicado: MDPI AG 2020-05-01
Series:Aerospace
Assuntos:
Acceso en liña:https://www.mdpi.com/2226-4310/7/5/62
Tags: Engadir etiqueta
Sen Etiquetas, Sexa o primeiro en etiquetar este rexistro!