FENSAP-ICE: A Second Generation 3D CFD-based In-Flight Icing Simulation System

Paper #:
  • 2003-01-2157

Published:
  • 2003-06-16
DOI:
  • 10.4271/2003-01-2157
Citation:
Habashi, W., Morency, F., and Beaugendre, H., "FENSAP-ICE: A Second Generation 3D CFD-based In-Flight Icing Simulation System," SAE Technical Paper 2003-01-2157, 2003, https://doi.org/10.4271/2003-01-2157.
Pages:
17
Abstract:
FENSAP-ICE is a second generation CFD-based in-flight icing simulation system, bringing to the icing field simulation advances widely used by the aircraft and turbo machinery industries. It is built in a modular and interlinked fashion to successively solve each of flow, impingement, accretion, heat loads and performance degradation via field models based on the Euler/Navier-Stokes equations for the clean and degraded flow, and new partial differential equations for the other three icing processes. This paper presents the FENSAP-ICE system and shows examples of its use to calculate impingement and ice shapes on a 3D helicopter rotor blade tip and on a nacelle inlet.
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