contributor author | O. E. Baljé | |
contributor author | R. L. Binsley | |
date accessioned | 2017-05-09T00:05:39Z | |
date available | 2017-05-09T00:05:39Z | |
date copyright | October, 1968 | |
date issued | 1968 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26671#341_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/125678 | |
description abstract | Generalized loss correlations for full and partial admission turbines have been derived and critically compared with recently published data. Effects included are Reynolds number, blade angles, blade height, blade number, blade trailing edge thickness, tip clearance, and reaction. These generalized loss relationships are for use in optimization of turbines over a wide range of possible operating conditions. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Axial Turbine Performance Evaluation. Part A—Loss-Geometry Relationships | |
type | Journal Paper | |
journal volume | 90 | |
journal issue | 4 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.3609211 | |
journal fristpage | 341 | |
journal lastpage | 348 | |
identifier eissn | 0742-4795 | |
keywords | Turbines | |
keywords | Geometry | |
keywords | Performance evaluation | |
keywords | Blades | |
keywords | Reynolds number | |
keywords | Clearances (Engineering) | |
keywords | Optimization AND Thickness | |
tree | Journal of Engineering for Gas Turbines and Power:;1968:;volume( 090 ):;issue: 004 | |
contenttype | Fulltext | |