contributor author | K. Takeishi | |
contributor author | K. Tsukagoshi | |
contributor author | S. Aoki | |
contributor author | T. Sato | |
date accessioned | 2017-05-08T23:39:50Z | |
date available | 2017-05-08T23:39:50Z | |
date copyright | October, 1992 | |
date issued | 1992 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28625#828_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/111047 | |
description abstract | The film cooling effectiveness on a low-speed stationary cascade and the rotating blade has been measured by using a heat-mass transfer analogy. The film cooling effectiveness on the suction surface of the rotating blade fits well with that on the stationary blade, but a low level of effectiveness appears on the pressure surface of the rotating blade. In this paper, typical film cooling data will be presented and film cooling on a rotating blade is discussed. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Film Cooling on a Gas Turbine Rotor Blade | |
type | Journal Paper | |
journal volume | 114 | |
journal issue | 4 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2928036 | |
journal fristpage | 828 | |
journal lastpage | 834 | |
identifier eissn | 1528-8900 | |
keywords | Cooling | |
keywords | Gas turbines | |
keywords | Rotors | |
keywords | Blades | |
keywords | Rotating blades | |
keywords | Suction | |
keywords | Cascades (Fluid dynamics) | |
keywords | Pressure AND Heat | |
tree | Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004 | |
contenttype | Fulltext | |