Three-Dimensional Numerical Simulation of Ice Accretion at the Engine Inlet
Author:
Affiliation:
1. School of Aeronautic Science and Engineering, Beihang University, 100191 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031992
Reference11 articles.
1. Icing Calculations on a Typical Commercial Jet Engine Inlet Nacelle
2. BidwellC. S.PotapczukM. G. “Users Manual for the NASA Lewis Three-Dimensional Ice Accretion Code (LEWICE3D),” NASA TM-105974, 1993.
3. FENSAP-ICE's Three-Dimensional In-Flight Ice Accretion Module: ICE3D
4. Comparison of Experimental and Computational Ice Shapes for an Engine Inlet
5. VeillardX.HabashiW. G.AubeM.BaruzziG. “FENSAP-ICE: Ice Accretion in Multi-stage Jet Engines,” AIAA Paper 2009-4158, 2009.
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