contributor author | R. Mani | |
contributor author | A. J. Acosta | |
date accessioned | 2017-05-09T00:06:14Z | |
date available | 2017-05-09T00:06:14Z | |
date copyright | April, 1968 | |
date issued | 1968 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26668#119_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/126012 | |
description abstract | A thin airfoil theory is developed for airfoils spanning a slowly diverging or converging channel, the motivation being to predict, theoretically, the effect of varying axial velocity on the cascade performance of axial flow compressor rows. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Quasi Two-Dimensional Flows Through a Cascade | |
type | Journal Paper | |
journal volume | 90 | |
journal issue | 2 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.3609146 | |
journal fristpage | 119 | |
journal lastpage | 127 | |
identifier eissn | 0742-4795 | |
keywords | Flow (Dynamics) | |
keywords | Cascades (Fluid dynamics) | |
keywords | Airfoils | |
keywords | Axial flow AND Channels (Hydraulic engineering) | |
tree | Journal of Engineering for Gas Turbines and Power:;1968:;volume( 090 ):;issue: 002 | |
contenttype | Fulltext | |