| contributor author | Alimohammadi, H. R. | |
| contributor author | Naseh, H. | |
| contributor author | Ommi, F. | |
| date accessioned | 2026-08-20T21:12:11Z | |
| date available | 2026-08-20T21:12:11Z | |
| date copyright | 2025/12/09 | |
| date issued | 2026 | |
| identifier other | JAEEEZ.ASENG-5307.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314105 | |
| 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 ... | |
| publisher | American Society of Civil Engineers | |
| title | New Framework for RBDO Applied in a Thrust Chamber | |
| type | Journal Article | |
| journal volume | 39 | |
| journal issue | 2 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/JAEEEZ.ASENG-5307 | |
| journal fristpage | 04025136-1 | |
| journal lastpage | 04025136-17 | |
| page | 17 | |
| tree | Journal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 002 | |
| contenttype | Fulltext | |
