Add to ORKGThe measurement of mass transfer from cavities is discussed with emphasis on the effect of cavity orientations relative to the main flow direction. A finite difference computation for turbulent air flow and heat transfer over a two-dimensional shrouded rectangular cavity is discussed
Steady simulations were performed to investigate tip leakage flow and heat transfer characteristics ...
Experimental investigations are performed to measure the detailed heat transfer coefficient and stat...
A combined computational and experimental study has been performed to investigate the detailed distr...
In gas turbines, the blades of axial turbine stages rotate in close proximity to a stationary periph...
Predictions of the rate of heat transfer to the tip and shroud of a gas turbine rotor blade are pres...
Local measurements of the heat transfer coefficient and pressure coefficient were conducted on the t...
ABSTRACT This work presents a numerical study that was done to investigate the heat transfer charact...
To improve the performance of aero-engines manufacturers strive to increase the inlet temperature to...
Qualitatively different heat transfer characteristics between a transonic blade tip and a subsonic o...
In this paper, the effect of cavity geometry of a squealer blade tip on its thermal performance is i...
In today's modern gas turbine engines, the region between the rotor and the stationary shroud has th...
ABSTRACT In enshrouded axial turbine stages, a small but generally unavoidable clearance between the...
The thermal performance of two cavity-winglet tips with endwall motion is investigated in a transoni...
One of the most critical components of gas turbine engines, rotor blade tip and casing, is exposed t...
The tips of unshrouded, high-pressure turbine blades are prone to significantly high heat loads. The...
Steady simulations were performed to investigate tip leakage flow and heat transfer characteristics ...
Experimental investigations are performed to measure the detailed heat transfer coefficient and stat...
A combined computational and experimental study has been performed to investigate the detailed distr...
In gas turbines, the blades of axial turbine stages rotate in close proximity to a stationary periph...
Predictions of the rate of heat transfer to the tip and shroud of a gas turbine rotor blade are pres...
Local measurements of the heat transfer coefficient and pressure coefficient were conducted on the t...
ABSTRACT This work presents a numerical study that was done to investigate the heat transfer charact...
To improve the performance of aero-engines manufacturers strive to increase the inlet temperature to...
Qualitatively different heat transfer characteristics between a transonic blade tip and a subsonic o...
In this paper, the effect of cavity geometry of a squealer blade tip on its thermal performance is i...
In today's modern gas turbine engines, the region between the rotor and the stationary shroud has th...
ABSTRACT In enshrouded axial turbine stages, a small but generally unavoidable clearance between the...
The thermal performance of two cavity-winglet tips with endwall motion is investigated in a transoni...
One of the most critical components of gas turbine engines, rotor blade tip and casing, is exposed t...
The tips of unshrouded, high-pressure turbine blades are prone to significantly high heat loads. The...
Steady simulations were performed to investigate tip leakage flow and heat transfer characteristics ...
Experimental investigations are performed to measure the detailed heat transfer coefficient and stat...
A combined computational and experimental study has been performed to investigate the detailed distr...