| contributor author | Ruban, Alex | |
| contributor author | Menezes, Viren | |
| contributor author | Balasubramanian, Sridhar | |
| contributor author | Srinivasan, K. | |
| date accessioned | 2022-02-04T21:58:54Z | |
| date available | 2022-02-04T21:58:54Z | |
| date copyright | 9/4/2020 12:00:00 AM | |
| date issued | 2020 | |
| identifier issn | 0098-2202 | |
| identifier other | fe_142_11_111211.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4274644 | |
| description abstract | This technical brief presents a flow separation mitigation device, called cavity-recirculator that can be used to control flow separation during shock wave–boundary layer interaction (SBLI) in high-speed intake flows. The cavity-recirculator isolates the flow separation bubble generated at the SBLI spot, thereby thinning the boundary layer and reducing the blockage of the inviscid stream in the duct. The device has a potential application in scramjet engine intakes/isolators. The cavity-recirculator was tested on a single-ramp-compression intake model in a hypersonic shock tunnel, in a freestream of Mach 8 (±0.1). The device operation and effectiveness were assessed by flow visualization and pressure measurements in the test model. The measurements and visualization displayed a mitigation of flow separation through an improved flow field with a single shock train and the absence of flow separation shock, in the inlet. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Shock–Boundary Layer-Interaction Control Through Recirculation in a Hypersonic Inlet | |
| type | Journal Paper | |
| journal volume | 142 | |
| journal issue | 11 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.4048141 | |
| journal fristpage | 0114502-1 | |
| journal lastpage | 0114502-8 | |
| page | 8 | |
| tree | Journal of Fluids Engineering:;2020:;volume( 142 ):;issue: 011 | |
| contenttype | Fulltext | |
