Validation of a Hot-Air Anti-icing Simulation Code Bombardier Aerospace

Format:

Conference/Event

Author/Creator:

Pueyo, A., author.

Conference Name:

World Aviation Congress & Exposition (2003-09-08 : Montreal, Canada)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2003

Summary:

This paper presents CHT2D, a 2D hot air anti-icing simulation tool developed by the Advanced Aerodynamics group of Bombardier Aerospace. The tool has been developed from two main modules: the ice prediction code CANICE and the Navier-Stokes solver NSU2D, which is used to solve the hot air internal flow. A "weak" coupling beween the two modules based on function calls and information exchange has been priviledged. Three validation test cases are presented: for dry air conditions. Predictions from CHT2D agree quite well with the experiments. Preliminary results are also presented for a test case in icing conditions for different heat loads from the anti-icing system, to study the effect on the accumulated ice

Notes:

Vendor supplied data

Publisher Number:

2003-01-3031

Access Restriction:

Restricted for use by site license