Set up your own cloud-native simulation in minutes.Start Simulating Now
0
0
1 Geometry
1 Mesh
1 Simulation setup
3 ResultsSteady-state thermal simulation of a rare-earth high-entropy oxide TBC system on a NACA 4412 turbine blade airfoil geometry. Four-layer coating system (Superalloy + Bond Coat + TGO + RE-HEO Topcoat) under engine operating conditions (1300°C hot gas, 900°C cooling side). Comparing thermal insulation performance of RE-HEO vs YSZ conventional coating.
by slilbaekslilbaek
kirubelmenberu created this project
19 days ago
1 Geometry 1 Mesh 1 Simulation setup 3 ResultsSteady-state thermal simulation of a rare-earth high-entropy oxide TBC system on a NACA 4412 turbine blade airfoil geometry. Four-layer coating system (Superalloy + Bond Coat + TGO + RE-HEO Topcoat) under engine operating conditions (1300°C hot gas, 900°C cooling side). Comparing thermal insulation performance of RE-HEO vs YSZ conventional coating.
