Waste heat recovery of an UAV propulsion system based on PEM fuel cell by a novel transcritical CO₂ - LNG hybrid cycle; thermodynamic and multiple linear regression analyses

Amir Hamzeh Farajollahia Department of Engineering, Imam Ali University, Tehran, IranCorrespondence[email protected]

https://orcid.org/0000-0001-9201-1871

Mustafa Musa Jaberb Dijlah University College, Baghdad, Iraq

Taleeb Zedan Tabanc Kut University College, Wasit, Iraq

Mohsen Rostamid Department of Mechanical Engineering, Babol Noshirvani University of Technology, Babol, Iran

Soheil Mousavid Department of Mechanical Engineering, Babol Noshirvani University of Technology, Babol, Iran

https://orcid.org/0000-0003-3813-4947

Tahere Jalalyd Department of Mechanical Engineering, Babol Noshirvani University of Technology, Babol, Iran

Mohanad Hatem Shadharb Dijlah University College, Baghdad, Iraq

show all

Citations (0)

Keep up to date with the latest research on this topic with citation updates for this article.

Reprints and Corporate Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

To request a reprint or corporate permissions for this article, please click on the relevant link below:

Order Reprints Request Corporate Permissions

Academic Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

Obtain permissions instantly via Rightslink by clicking on the button below:

Request Academic Permissions

If you are unable to obtain permissions via Rightslink, please complete and submit this Permissions form. For more information, please visit our Permissions help page.

Waste heat recovery of an UAV propulsion system based on PEM fuel cell by a novel transcritical CO₂ - LNG hybrid cycle; thermodynamic and multiple linear regression analyses

Information for

Open access

Opportunities

Help and information

Your download is now in progress and you may close this window

Login or register to access this feature

Waste heat recovery of an UAV propulsion system based on PEM fuel cell by a novel transcritical CO2 - LNG hybrid cycle; thermodynamic and multiple linear regression analyses

Citations (0)

Reprints and Corporate Permissions

Academic Permissions

Related research

To cite this article:

Download citation

Information for

Open access

Opportunities

Help and information

Keep up to date

Waste heat recovery of an UAV propulsion system based on PEM fuel cell by a novel transcritical CO₂ - LNG hybrid cycle; thermodynamic and multiple linear regression analyses