| contributor author | Kung-Ming Chung | |
| contributor author | Associate Research Fellow | |
| date accessioned | 2017-05-09T00:05:18Z | |
| date available | 2017-05-09T00:05:18Z | |
| date copyright | March, 2001 | |
| date issued | 2001 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-27160#139_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/125469 | |
| description abstract | Experiments are performed to study the interaction of an impinging shock wave and an expansion fan in a Mach 1.280 flow. The expansion fan neutralizes the pressure rise induced by the impinging shock wave. The mean surface static pressure shows a linear combination of the effect of both perturbations. Surface pressure fluctuations, which are associated with the characteristics of the perturbed boundary layer, indicate a transitional behavior. This is related to a nonlinear phenomenon arising the simultaneous action of the impinging shock wave and the expansion fan. The level of downstream pressure fluctuation depends on the overall inviscid interaction strength. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Investigation on Turbulent Expansion-Corner Flow With Shock Impingement | |
| type | Journal Paper | |
| journal volume | 123 | |
| journal issue | 1 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.1343084 | |
| journal fristpage | 139 | |
| journal lastpage | 144 | |
| identifier eissn | 1528-901X | |
| keywords | Pressure | |
| keywords | Flow (Dynamics) | |
| keywords | Turbulence | |
| keywords | Shock waves | |
| keywords | Shock (Mechanics) | |
| keywords | Corners (Structural elements) | |
| keywords | Boundary layers AND Fluctuations (Physics) | |
| tree | Journal of Fluids Engineering:;2001:;volume( 123 ):;issue: 001 | |
| contenttype | Fulltext | |
