| dc.contributor.author | Qiu, Bo | |
| dc.contributor.author | Zhu, Yandan | |
| dc.contributor.author | Liu, Xiao | |
| dc.contributor.author | Zhang, Haoyuan | |
| dc.contributor.author | Yao, Jie | |
| dc.contributor.author | Zeng, Lei | |
| dc.date.accessioned | 2026-08-20T21:12:57Z | |
| dc.date.available | 2026-08-20T21:12:57Z | |
| dc.date.copyright | 2025/07/10 | |
| dc.date.issued | 2025 | |
| dc.identifier.other | JAEEEZ.ASENG-6113.pdf | |
| dc.identifier.uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314125 | |
| dc.description.abstract | AbstractAiming at the coupling problem between the aerothermal environment of an aircraft’s
flow field and the thermal response of its structural field, this paper proposes a
novel coupling calculation method based on whole ballistic iteration, which ... | |
| dc.publisher | American Society of Civil Engineers | |
| dc.title | Aerothermal–Heat Transfer Coupling Calculation Method Based on Whole Ballistic Iteration | |
| 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-6113 | |
| dc.journal.fristpage | 04025072-1 | |
| dc.journal.lastpage | 04025072-15 | |
| dc.page | 15 | |
| dc.tree | Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005 | |
| dc.contenttype | Fulltext | |
