New Framework for RBDO Applied in a Thrust Chamber

dc.contributor.author	Alimohammadi, H. R.
dc.contributor.author	Naseh, H.
dc.contributor.author	Ommi, F.
dc.date.accessioned	2026-08-20T21:12:11Z
dc.date.available	2026-08-20T21:12:11Z
dc.date.copyright	2025/12/09
dc.date.issued	2026
dc.identifier.other	JAEEEZ.ASENG-5307.pdf
dc.identifier.uri	http://yetl.yabesh.ir/yetl1/handle/yetl/4314105
dc.description.abstract	AbstractThe design of a thrust chamber (TC) of a liquid propellant engine (LPE) presents several challenges from performance to predicting the optimization and reliability of the TC. Thus, multidisciplinary reliability-based design optimization (MMRBDO) ...Practical ApplicationsOne of the major challenges of large industries (automotive, aerospace, and space industries) is the design of systems with various disciplines with optimization and reliability considerations. To address this challenge, modern ...
dc.publisher	American Society of Civil Engineers
dc.title	New Framework for RBDO Applied in a Thrust Chamber
dc.type	Journal Article
dc.journal.volume	39
dc.journal.issue	2
dc.journal.title	Journal of Aerospace Engineering
dc.identifier.doi	10.1061/JAEEEZ.ASENG-5307
dc.journal.fristpage	04025136-1
dc.journal.lastpage	04025136-17
dc.page	17
dc.tree	Journal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 002
dc.contenttype	Fulltext