Multi-time Step Icing Calculations Using a 3D Multi-block Structured Mesh Generation Procedure 2015-01-2161
The 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.
Citation: Hasanzadeh, K., Pena, D., Hoarau, Y., and Laurendeau, E., "Multi-time Step Icing Calculations Using a 3D Multi-block Structured Mesh Generation Procedure," SAE Technical Paper 2015-01-2161, 2015, https://doi.org/10.4271/2015-01-2161. Download Citation
Author(s):
Kazem Hasanzadeh, Dorian Pena, Yannick Hoarau, Eric Laurendeau
Affiliated:
Ecole Polytechnique Montreal, Strasbourg University
Pages: 13
Event:
SAE 2015 International Conference on Icing of Aircraft, Engines, and Structures
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Icing and ice detection
Simulation and modeling
Wings
Thermodynamics
Windows and windshields
Glass
Logistics
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