| contributor author | Lv, Zheng | |
| contributor author | Ye, Tao | |
| contributor author | Ding, Haipeng | |
| date accessioned | 2026-08-20T21:12:31Z | |
| date available | 2026-08-20T21:12:31Z | |
| date copyright | 2026/05/28 | |
| date issued | 2026 | |
| identifier other | JAEEEZ.ASENG-6030.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314117 | |
| 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 ... | |
| publisher | American Society of Civil Engineers | |
| title | Design and Investigation of a Three-Dimensional TBCC Exhaust System Operating at Mach 0–6 | |
| type | Journal Article | |
| journal volume | 39 | |
| journal issue | 5 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/JAEEEZ.ASENG-6030 | |
| journal fristpage | 04026029-1 | |
| journal lastpage | 04026029-17 | |
| page | 17 | |
| tree | Journal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 005 | |
| contenttype | Fulltext | |
