Icing modelling in NSMB with chimera overset grids
Author(s) -
Dorian Pena,
Thibaut Deloze,
Éric Laurendeau,
Yannick Hoarau
Publication year - 2015
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.4912351
Subject(s) - icing , solver , computer science , eulerian path , computational science , aerospace engineering , aerospace , simulation , lagrangian , meteorology , engineering , physics , programming language , mathematical physics
In aerospace Engineering, the accurate simulation of ice accretion is a key element to increase flight safety and avoid accidents related to icing effects. The icing code developed in the NSMB solver is based on an Eulerian formulation for droplets tracking, an iterative Messinger model using a modified water runback scheme for ice thickness calculation and mesh deformation to track the ice/air interface through time. The whole process is parallelized with MPI and applied with chimera grids.
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