| contributor author | M. H. Williams | |
| date accessioned | 2017-05-08T23:14:46Z | |
| date available | 2017-05-08T23:14:46Z | |
| date copyright | June, 1983 | |
| date issued | 1983 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-26217#275_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/96652 | |
| description abstract | The effect of a standing shock wave on the static and dynamic aeroelastic stability of a flexible panel is investigated using a linear structural and aerodynamic theoretical model. It is found that the shock is generally stabilizing. The lowest critical dynamic pressures are associated with shock positions downstream from the panel, where the panel is uninfluenced by the shock. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Effect of a Normal Shock on the Aeroelastic Stability of a Panel | |
| type | Journal Paper | |
| journal volume | 50 | |
| journal issue | 2 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3167032 | |
| journal fristpage | 275 | |
| journal lastpage | 282 | |
| identifier eissn | 1528-9036 | |
| keywords | Stability | |
| keywords | Shock (Mechanics) AND Shock waves | |
| tree | Journal of Applied Mechanics:;1983:;volume( 050 ):;issue: 002 | |
| contenttype | Fulltext | |
