Multi-time Step Icing Calculations Using a 3D Multi-block Structured Mesh Generation Procedure Ecole Polytechnique Montreal

Format:

Conference/Event

Author/Creator:

Hasanzadeh, Hasanzadeh, author.

Contributor:

Hoarau, Yannick

Laurendeau, Eric

Pena, Dorian

Conference Name:

SAE 2015 International Conference on Icing of Aircraft, Engines, and Structures (2015-06-22 : Prague, Czech Republic)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2015

Summary:

AbstractThe paper presents the framework of fully automated two/three dimensional ice accretion simulation package, with emphasis on the remeshing step. The NSMB3D-ICE Navier-Stokes code, coupled to an Eulerian droplet module and iterative Messinger thermodynamic model, can perform multi time-steps ice accretion simulations via an automated multi-block elliptic/parabolic grid generation code (NSGRID3D). Attention is paid to the efficiency and robustness of the numerical calculations especially for complex 3D glaze ice simulation. The new automated multi time-step icing code NSMB3D-ICE/NSGRID3D is used to compute several icing studies on the GLC305 wing for rime and glaze ice cases

Notes:

Vendor supplied data

Publisher Number:

2015-01-2161

Access Restriction:

Restricted for use by site license