A mechanical model to investigate airfoil de-icing mechanics
A mechanical model to investigate airfoil de-icing mechanics
- Neue Suche nach: Kermanidis, T.B.
- Neue Suche nach: Lentzos, G.A.
- Neue Suche nach: Pantelakis, S.G.
- Neue Suche nach: Hammond, D.W.
- Neue Suche nach: Kermanidis, T.B.
- Neue Suche nach: Lentzos, G.A.
- Neue Suche nach: Pantelakis, S.G.
- Neue Suche nach: Hammond, D.W.
A fracture mechanical model for the prediction of the ice detachment from an elastic sheet subjected to dynamic loading is proposed. The mechanical model consists of an one dimensional linear elastic beam covered with an ice layer and an interfacial crack between the two layers. Finite element analysis and experimental observations on a partially covered ice clad aluminium alloy plate, fitted with an Electro-Impulsive De-Icer werde used to support the modelling and to identify the criteria which most influence the de-icing process. The proposed approach has resulted to a good correlation between experimentally obtained de-icing process and the model's prediction.
Dokumentinformationen
A mechanical model to investigate airfoil de-icing mechanics
Ein mechanisches Modell zur Untersuchung der Tragflügel-Enteisungsmechanik
Zeitschrift für Flugwissenschaften und Weltraumforschung ; 19 , 4 ; 299-306
1995
8 Seiten, 16 Bilder, 1 Tabelle, 9 Quellen
Aufsatz (Zeitschrift)
Englisch
Flugzeug , Tragflügel , Bruchmechanik , Vereisung , Aluminiumlegierung , Enteisen , Impuls , Rissausbreitung , Grenzfläche , Wechsellast (mechanisch) , Korrelation , Finite-Elemente-Methode , Variationsrechnung , Software , analytische Untersuchung , praktische Untersuchung , elektromagnetischer Impuls
Ähnliche Titel
A mechanical model to investigate airfoil de-icing mechanics.
| Online Contents | 1995
Icing Research for Airfoil and Multi-Element Airfoil
| British Library Conference Proceedings | 2006
Prop-fan airfoil icing characteristics
| AIAA | 1989
Airfoil aerodynamics in icing conditions
| AIAA | 1986
Icing Research for Airfoil and Multi-Element Airfoil
| AIAA | 2006