Extension to the Messinger model for aircraft icing
Extension to the Messinger model for aircraft icing
- Neue Suche nach: Myers, T.G.
- Neue Suche nach: Myers, T.G.
A one-dimensional mathematical model is developed describing ice growth due to supercooled fluid impacting on a solid substrate. When rime ice forms, the ice thickness is determined by a simple mass balance. The leading-order temperature profile through the ice is then obtained as a function of time, the ambient conditions, and the ice thickness. When glaze ice forms, the energy equation and mass balance are combined to provide a single first order nonlinear differential equation for the ice thickness, which is solved numerically. Once the ice thickness is obtained, the water height and the temperatures in the layers may be calculated. The method for extending the one-dimensional model to two and three dimensions is described. Ice growth rates and freezing fractions predicted by the current method are compared with the Messinger model. The Messinger model is shown to be a Iimiting case for the present method.
Dokumentinformationen
Extension to the Messinger model for aircraft icing
Erweiterung des Messinger-Modells für die Vereisung von Flugzeugen
AIAA Journal ; 39 , 2 ; 211-218
2001
8 Seiten, 6 Bilder, 1 Tabelle, 24 Quellen
Aufsatz (Zeitschrift)
Englisch
Ähnliche Titel
Extension to the Messinger Model for Aircraft Icing
| AIAA | 2001
FLUID DYNAMICS - Extension to the Messinger Model for Aircraft Icing
| Online Contents | 2001
Messinger specialists in hazchems
British Library Online Contents | 1996
| DOAJ | 2023