Prediction of three-dimensional flow field and heat transfer in a two pass rib-roughened square internal cooling channel of turbine blades with rounded staggered ribs rotating at high rotation and density ratios is the main focus of this study. Rotation, buoyancy, ribs, and geometry affect the flow within these channels. The full two-pass channel with bend and with rounded staggered ribs with fillets (e/Dh =0.1 and P/e=10) as tested by Wagner et. al [1992] is investigated. RSM is used in this study and enhanced wall treatment approach to resolve the near wall viscosity-affected region. RSM model was validated against available experimental data (which are primarily at low rotation and buoyancy numbers). The model was then used for cases wit...
This study attempts to understand one of the most fundamental and challenging problems in fluid flow...
The present investigation emphases on rotation effects on internal cooling of gas turbine blades bot...
The flow field inside a triangular cooling channel for the leading edge of a gas turbin...
Prediction of three-dimensional flow field and heat transfer in a two pass rib-roughened square inte...
Prediction of three-dimensional flow field and heat transfer in a two pass rib-roughened square inte...
Numerical simulation of fluid flow and heat transfer for high rotation and buoyancy numbers flow in ...
Numerical simulation of fluid flow and heat transfer of high rotation and density ratio flow in inte...
Prediction of flow field and heat transfer of high rotation numbers and density ratio flow in a squa...
Prediction of flow field and heat transfer of high rotation numbers and density ratio flow in a squa...
Prediction of flow field and heat transfer of high rotation numbers and density ratio flow in a squa...
Purpose: The study aims to focus on rotation effects on a ribbed channel of gas turbine blades for i...
This study attempts to understand one of the most fundamental and challenging problems in fluid flow...
This study attempts to understand one of the most fundamental and challenging problems in fluid flow...
The flow field inside a triangular cooling channel for the leading edge of a gas turbine blade has b...
This study attempts to understand one of the most fundamental and challenging problems in fluid flow...
This study attempts to understand one of the most fundamental and challenging problems in fluid flow...
The present investigation emphases on rotation effects on internal cooling of gas turbine blades bot...
The flow field inside a triangular cooling channel for the leading edge of a gas turbin...
Prediction of three-dimensional flow field and heat transfer in a two pass rib-roughened square inte...
Prediction of three-dimensional flow field and heat transfer in a two pass rib-roughened square inte...
Numerical simulation of fluid flow and heat transfer for high rotation and buoyancy numbers flow in ...
Numerical simulation of fluid flow and heat transfer of high rotation and density ratio flow in inte...
Prediction of flow field and heat transfer of high rotation numbers and density ratio flow in a squa...
Prediction of flow field and heat transfer of high rotation numbers and density ratio flow in a squa...
Prediction of flow field and heat transfer of high rotation numbers and density ratio flow in a squa...
Purpose: The study aims to focus on rotation effects on a ribbed channel of gas turbine blades for i...
This study attempts to understand one of the most fundamental and challenging problems in fluid flow...
This study attempts to understand one of the most fundamental and challenging problems in fluid flow...
The flow field inside a triangular cooling channel for the leading edge of a gas turbine blade has b...
This study attempts to understand one of the most fundamental and challenging problems in fluid flow...
This study attempts to understand one of the most fundamental and challenging problems in fluid flow...
The present investigation emphases on rotation effects on internal cooling of gas turbine blades bot...
The flow field inside a triangular cooling channel for the leading edge of a gas turbin...