| contributor author | G. N. Balaji | |
| contributor author | J. H. Griffin | |
| date accessioned | 2017-05-08T23:53:33Z | |
| date available | 2017-05-08T23:53:33Z | |
| date copyright | January, 1997 | |
| date issued | 1997 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26761#147_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/118735 | |
| description abstract | The resonant response characteristics of a tapered beam are studied using Euler–Bernoulli beam theory. The sensitivity of the beam’s maximum stress to variations in its geometry is studied for three types of harmonic pressure loading. The implications to the response of airfoil chordwise bending modes are discussed. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Resonant Response of a Tapered Beam and Its Implications to Blade Vibration | |
| type | Journal Paper | |
| journal volume | 119 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2815539 | |
| journal fristpage | 147 | |
| journal lastpage | 152 | |
| identifier eissn | 0742-4795 | |
| keywords | Pressure | |
| keywords | Stress | |
| keywords | Vibration | |
| keywords | Blades | |
| keywords | Geometry AND Airfoils | |
| tree | Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 001 | |
| contenttype | Fulltext | |
