Ice Crystals Trajectory Calculations in a Turbofan Engine
Author:
Affiliation:
1. Safran Group
2. ONERA
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4130
Reference21 articles.
1. Glaciated and mixed phase ice accretion modeling using ONERA 2D icing suite
2. A comprehensive numerical model for mixed-phase and glaciated icing conditions
3. Experimental and numerical investigations on aircraft icing at mixed phase conditions
4. Eulerian and Lagrangian Ice-Crystal Trajectory Simulations in a Generic Turbofan Compressor
5. Large-Eddy Simulation of Kerosene Spray Ignition in a Simplified Aeronautic Combustor
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3. Numerical Simulation of In-Flight Icing in Jet Engines;Handbook of Numerical Simulation of In-Flight Icing;2023-12-12
4. Numerical Simulation of Ice Crystals and Mixed-Phase In-Flight Icing Conditions;Handbook of Numerical Simulation of In-Flight Icing;2023-12-12
5. Numerical Simulation of Ice Crystals Growth in Turbofan Engines;Handbook of Numerical Simulation of In-Flight Icing;2023-12-12
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