Transient Response of Three-Layered RingsSource: Journal of Applied Mechanics:;1977:;volume( 044 ):;issue: 002::page 299Author:M. J. Sagartz
DOI: 10.1115/1.3424041Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Hamilton’s principle is used to derive equations of motion for a linear elastic three-layered ring. The theory includes the effects of shear deformation and rotatory inertia in each layer and radial strain effects in the middle layer. A convenient computational technique is developed for transient response evaluation. A companion experimental study was conducted using two different rings. Both rings had aluminum inner and outer layers, but each had a different low-modulus middle layer. Radial impulse loads distributed as a cosine over half the ring circumference, were applied to the outer ring surface, and the transient response was monitored with strain gages mounted on the aluminum layers. Measured strain-time histories were compared with theoretical calculations, and good agreement was obtained.
keyword(s): Transients (Dynamics) , Aluminum , Stress , Inertia (Mechanics) , Equations of motion , Impulse (Physics) , Hamilton's principle , Shear deformation AND Strain gages ,
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| contributor author | M. J. Sagartz | |
| date accessioned | 2017-05-08T23:02:21Z | |
| date available | 2017-05-08T23:02:21Z | |
| date copyright | June, 1977 | |
| date issued | 1977 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-26072#299_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/89554 | |
| description abstract | Hamilton’s principle is used to derive equations of motion for a linear elastic three-layered ring. The theory includes the effects of shear deformation and rotatory inertia in each layer and radial strain effects in the middle layer. A convenient computational technique is developed for transient response evaluation. A companion experimental study was conducted using two different rings. Both rings had aluminum inner and outer layers, but each had a different low-modulus middle layer. Radial impulse loads distributed as a cosine over half the ring circumference, were applied to the outer ring surface, and the transient response was monitored with strain gages mounted on the aluminum layers. Measured strain-time histories were compared with theoretical calculations, and good agreement was obtained. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Transient Response of Three-Layered Rings | |
| type | Journal Paper | |
| journal volume | 44 | |
| journal issue | 2 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3424041 | |
| journal fristpage | 299 | |
| journal lastpage | 304 | |
| identifier eissn | 1528-9036 | |
| keywords | Transients (Dynamics) | |
| keywords | Aluminum | |
| keywords | Stress | |
| keywords | Inertia (Mechanics) | |
| keywords | Equations of motion | |
| keywords | Impulse (Physics) | |
| keywords | Hamilton's principle | |
| keywords | Shear deformation AND Strain gages | |
| tree | Journal of Applied Mechanics:;1977:;volume( 044 ):;issue: 002 | |
| contenttype | Fulltext |