Zobrazeno 1 - 10
of 29
pro vyhledávání: '"Zoheir Saboohi"'
Publikováno v:
Results in Engineering, Vol 23, Iss , Pp 102495- (2024)
In this article, a systematic approach is presented for simulating turbojet engine performance at both design and off-design points. The construction of gas turbine engines involves a core, with additional components added based on the proposed metho
Externí odkaz:
https://doaj.org/article/dbcdff5941b44c64a1043f911e818ac5
Publikováno v:
Case Studies in Thermal Engineering, Vol 53, Iss , Pp 103836- (2024)
In this article, the heat transfers and ablation phenomena of thermal insulations utilized in manned space capsules are investigated. In this regard, by collecting and solving the equations related to ablation insulations, a computer program has been
Externí odkaz:
https://doaj.org/article/0d8bc7474e00429b93b0a500ad17f845
Publikováno v:
مهندسی مکانیک شریف, Vol 38.3, Iss 1, Pp 113-125 (2022)
This paper presents a numerical method to evaluate the system conditions in transient mode for a standing wave thermo-acoustic engine (STAE). This method focuses on increasing the accuracy of predictions and creating a better eyesight of the operatin
Externí odkaz:
https://doaj.org/article/826c4f967b1a42449b3a256af12edae0
Publikováno v:
Hydrogen, Fuel Cell & Energy Storage, Vol 8, Iss 2, Pp 103-112 (2021)
One of the most important methods for efficient hydrogen utilization is the proton exchange membrane fuel cell (PEMFC) because of its low environmental impact and easy maintenance. Depletion of fossil fuels along with global warming is all the more r
Externí odkaz:
https://doaj.org/article/205095d60c5549179c8b1310fd589cec
Autor:
Zoheir Saboohi
Publikováno v:
فصلنامه علوم و فناوری فضایی, Vol 12, Iss 3, Pp 1-13 (2019)
In this paper, the design of a diffuser for a suction type subsonic wind tunnel equipped with three axial fans has been taken into account by CFD. The tunnel test section has a 140 cm height and 195cm width. For numerical modeling the axial fans that
Externí odkaz:
https://doaj.org/article/bdf7c1a5a21749cf8c1a97471ac33b6d
Publikováno v:
فصلنامه علوم و فناوری فضایی, Vol 12, Iss 1, Pp 23-40 (2019)
Micro-propulsion Systems are low thrust engines that be used in space missions like keeping satellite in orbit and changing orbit. These engines have several kinds and liquid propellant micro-propulsion is used in this project. In two propellant micr
Externí odkaz:
https://doaj.org/article/32521df8b5df425191f99a340c38cc84
Publikováno v:
Heat and Mass Transfer. 58:2175-2193
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c87ffc8556cf943411314fb1b022ac9e
https://doi.org/10.1007/s00231-022-03235-w
https://doi.org/10.1007/s00231-022-03235-w
Publikováno v:
Journal of The Institution of Engineers (India): Series C. 103:421-434
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9ec5aae5539dbcc9ba1e306eaf02f3ac
https://doi.org/10.1007/s40032-021-00780-x
https://doi.org/10.1007/s40032-021-00780-x
Autor:
Zoheir Saboohi, Fathollah Ommi, Ebrahim Rahmani, Tofigh Moradi, Abolfazl Fattahi, Mostafa Delpisheh, Nader Karimi
Publikováno v:
Chemical Engineering Communications. 210:773-787
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e3277b1bdea9c679a72499f82e48bb2e
https://doi.org/10.1080/00986445.2022.2026338
https://doi.org/10.1080/00986445.2022.2026338
