| dc.contributor.author | Yang, Jiawei | |
| dc.contributor.author | Wu, Zeping | |
| dc.contributor.author | Wang, Wenjie | |
| dc.contributor.author | Zhang, Weihua | |
| dc.date.accessioned | 2026-08-20T21:12:00Z | |
| dc.date.available | 2026-08-20T21:12:00Z | |
| dc.date.copyright | 2025/07/25 | |
| dc.date.issued | 2025 | |
| dc.identifier.other | JAEEEZ.ASENG-5120.pdf | |
| dc.identifier.uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314103 | |
| dc.description.abstract | AbstractSolid rocket motor design based on high-fidelity simulation models is extremely time-consuming
in practical engineering problems. To improve the efficiency of solid rocket motor
design problems, this study proposes a multifidelity model–assisted ... | |
| dc.publisher | American Society of Civil Engineers | |
| dc.title | Multifidelity Model–Assisted Knowledge Transfer Optimization Method for Computationally Intensive Solid Rocket Motor Design | |
| dc.type | Journal Article | |
| dc.journal.volume | 38 | |
| dc.journal.issue | 6 | |
| dc.journal.title | Journal of Aerospace Engineering | |
| dc.identifier.doi | 10.1061/JAEEEZ.ASENG-5120 | |
| dc.journal.fristpage | 04025078-1 | |
| dc.journal.lastpage | 04025078-14 | |
| dc.page | 14 | |
| dc.tree | Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006 | |
| dc.contenttype | Fulltext | |
