| dc.contributor.author | Lv, Zheng | |
| dc.contributor.author | Ye, Tao | |
| dc.contributor.author | Ding, Haipeng | |
| dc.date.accessioned | 2026-08-20T21:12:31Z | |
| dc.date.available | 2026-08-20T21:12:31Z | |
| dc.date.copyright | 2026/05/28 | |
| dc.date.issued | 2026 | |
| dc.identifier.other | JAEEEZ.ASENG-6030.pdf | |
| dc.identifier.uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314117 | |
| dc.description.abstract | AbstractThis study presents the design and investigation of a three-dimensional (3D) turbine-based
combined cycle (TBCC) exhaust system operating across Mach 0 to 6. The streamline
tracing technique is utilized to design the 3D asymmetric nozzle for the ... | |
| dc.publisher | American Society of Civil Engineers | |
| dc.title | Design and Investigation of a Three-Dimensional TBCC Exhaust System Operating at Mach 0–6 | |
| dc.type | Journal Article | |
| dc.journal.volume | 39 | |
| dc.journal.issue | 5 | |
| dc.journal.title | Journal of Aerospace Engineering | |
| dc.identifier.doi | 10.1061/JAEEEZ.ASENG-6030 | |
| dc.journal.fristpage | 04026029-1 | |
| dc.journal.lastpage | 04026029-17 | |
| dc.page | 17 | |
| dc.tree | Journal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 005 | |
| dc.contenttype | Fulltext | |
