This paper provides an immersed boundary method using a flexible local grid refinement technique for solving conjugate-heat-transfer problems. The proposed method is used to solve the flow past a heated hollow cylinder inside a channel together with the temperature field within the cylinder and then to predict turbomachinery blade cooling.
Volume Subject Area:
3rd Joint US-European Fluids Engineering Summer Meeting
Topics:
Blades,
Cooling,
Cylinders,
Flow (Dynamics),
Heat,
Heat transfer,
Temperature,
Turbomachinery
This content is only available via PDF.
Copyright © 2010
by ASME
You do not currently have access to this content.
