Computational Eulerian- Eulerian Analysis of In-Flight Icing

Name: Computational Eulerian- Eulerian Analysis of In-Flight Icing
Brand: LAP Lambert Academic Publishing
SKU: 9783838325521
Price: 235.21 RON
Availability: InStock

Water Droplets Impingement on a Convair-580 Nose and Cockpit Geometry

Autor: Ziad Boutanios

Limbă:

Legare: Carte broșată

Editura: LAP Lambert Academic Publishing

Disponibilitate: În depozitul extern

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In-flight icing occurs mostly during airplane take-off and approach where the airplane ground speed...

Informații despre carte

Autor

Ziad Boutanios

Limbă

engleză

Legare

Carte - Carte broșată

Publicat

2009

Pagini

EAN

9783838325521

Enbook ID

06890438

Editura

LAP Lambert Academic Publishing

Greutate

119

Dimensiuni

150 x 220 x 4

Descriere completă

In-flight icing occurs mostly during airplane take-off and approach where the airplane ground speed is still low enough to permit ice accretion, due to supercooled water droplets impingement. If unaddressed, such occurrences can be fatal. The problem is compounded by the large power requirements during take-off and landing which might affect the ice protection systems performance adversely. In this work, the Eulerian-Eulerian 3-D approach to calculating water droplet impingement is presented, with validation results in both 2-D and 3-D. A 3-D analysis is also carried out over a Convair-580 nose and cockpit geometry. This full-scale 3-D analysis is a simulation of a flight segment of the Canadian Freezing Drizzle Experiment as conducted by the Atmospheric Environment Services. Special emphasis is given to side window impingement on the Convair-580. The advantages of the Eulerian approach over the classical Lagrangian approach are also discussed.

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Computational Eulerian- Eulerian Analysis of In-Flight Icing

Water Droplets Impingement on a Convair-580 Nose and Cockpit Geometry

Informații despre carte

Descriere completă

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