A depth-averaged model for non-isothermal thin-film rimming flow

Keyphrases

• Aeroengine Bearing 50%
• Bearing Chamber 50%
• Boundary Temperature 50%
• Circular Cylinder 50%
• Convective Effects 50%
• Depth-averaged 50%
• Depth-averaged Model 100%
• Flow Configuration 50%
• Heat Convection 50%
• Inside Surface 50%
• Rimming Flow 100%
• Shear-driven 50%
• Steep Front 50%

Engineering

• Boundary Temperature 33%
• Convective Effect 33%
• Flow Configuration 33%
• Inside Surface 33%