| dc.contributor.author | Oqaz, Pouria Mohamadzadeh | |
| dc.contributor.author | Abedian, Ali | |
| dc.contributor.author | Tashi, Samaneh | |
| dc.date.accessioned | 2026-08-20T21:12:14Z | |
| dc.date.available | 2026-08-20T21:12:14Z | |
| dc.date.copyright | 2026/05/24 | |
| dc.date.issued | 2026 | |
| dc.identifier.other | JAEEEZ.ASENG-5448.pdf | |
| dc.identifier.uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314106 | |
| dc.description.abstract | AbstractToday, more than 50 weight percent of the structure of advanced civil aircraft such
as the B787 and the A350 are made up of composite materials. Even large parts such
as these planes’ wing spars and fuselage are composites, and in the case of any ... | |
| dc.publisher | American Society of Civil Engineers | |
| dc.title | Scarf Repair Design Based on the Axiomatic Design Approach | |
| 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-5448 | |
| dc.journal.fristpage | 04026026-1 | |
| dc.journal.lastpage | 04026026-14 | |
| dc.page | 14 | |
| dc.tree | Journal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 005 | |
| dc.contenttype | Fulltext | |
