| dc.contributor.author | Ukai, Takahiro | |
| dc.contributor.author | Kishida, Takahiro | |
| dc.contributor.author | Takioka, Ryo | |
| dc.date.accessioned | 2026-08-20T21:13:14Z | |
| dc.date.available | 2026-08-20T21:13:14Z | |
| dc.date.copyright | 2025/06/04 | |
| dc.date.issued | 2025 | |
| dc.identifier.other | JAEEEZ.ASENG-6211.pdf | |
| dc.identifier.uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314135 | |
| dc.description.abstract | AbstractA Mach 2.6 jet was manipulated by a steady Mach 2.0 injected at different angles within
the range of θ=30° and 90° at 20° intervals. This study aims to understand the effects of the injection
angle on the manipulated supersonic jet impinging on a ... | |
| dc.publisher | American Society of Civil Engineers | |
| dc.title | Flow Structure Manipulation in a Supersonic Jet Impinging on a Perpendicular Flat Plate with Varied Fluidic Injection Angles | |
| dc.type | Journal Article | |
| dc.journal.volume | 38 | |
| dc.journal.issue | 5 | |
| dc.journal.title | Journal of Aerospace Engineering | |
| dc.identifier.doi | 10.1061/JAEEEZ.ASENG-6211 | |
| dc.journal.fristpage | 04025062-1 | |
| dc.journal.lastpage | 04025062-8 | |
| dc.page | 8 | |
| dc.tree | Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005 | |
| dc.contenttype | Fulltext | |
