contributor author | A. W. Leissa | |
contributor author | J. K. Lee | |
contributor author | A. J. Wang | |
date accessioned | 2017-05-08T23:13:15Z | |
date available | 2017-05-08T23:13:15Z | |
date copyright | April, 1982 | |
date issued | 1982 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26772#296_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/95790 | |
description abstract | Shallow shell theory and Ritz method are employed to determine the frequencies and mode shapes of turbomachinery blades having both camber and twist, rotating with non-zero angles of attack. Frequencies obtained for different degrees of shallowness and thickness are compared with results available in the literature, obtained from finite element analyses of nonrotating blades. Frequencies are also determined for a rotating blade, showing the effects of changing the (1) angular velocity of rotation (2) disk radius and (3) angle of attack, as well as the significance of the most important body force terms. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Rotating Blade Vibration Analysis Using Shells | |
type | Journal Paper | |
journal volume | 104 | |
journal issue | 2 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.3227279 | |
journal fristpage | 296 | |
journal lastpage | 302 | |
identifier eissn | 0742-4795 | |
keywords | Shells | |
keywords | Rotating blades | |
keywords | Vibration analysis | |
keywords | Frequency | |
keywords | Blades | |
keywords | Shapes | |
keywords | Thickness | |
keywords | Turbomachinery | |
keywords | Force | |
keywords | Rotation | |
keywords | Finite element analysis AND Disks | |
tree | Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002 | |
contenttype | Fulltext | |