Advanced Thermal Management in Aerospace Systems

A special issue of Aerospace (ISSN 2226-4310).

Deadline for manuscript submissions: 31 March 2026 | Viewed by 18

Special Issue Editors


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Guest Editor
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, 29 Yudao St., Nanjing 210016, China
Interests: aircraft environmental control; avionics cooling; thermal control; aircraft air conditioning; boiling heat transfer; condensing heat transfer; multiphase flow; flow resistance
Special Issues, Collections and Topics in MDPI journals

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Guest Editor
Department of Modern Mechanics, University of Science and Technology of China, 96 Jinzhai Road, Hefei 230026, China
Interests: active thermal protection of aerospace vehicles; avionics cooling, boiling heat transfer; supercritical fluid enhanced heat transfer; micro/nano-structured surface enhanced heat transfer

Special Issue Information

Dear Colleagues, 

In aerospace systems, thermal management plays an increasingly important role. Thermal management systems integrate power and thermal management systems (PTMSs), fuel thermal management systems (FTMSs), engine systems, and flight vehicle structure systems. PTMSs may include secondary power systems, engine starting systems, environmental control systems, thermal control systems, anti-/de-icing systems, hydraulic systems, and lubrication systems. The FTMS not only provides fuel for the engine to produce power, but it may also use fuel as the heat sinks of the environmental control, hydraulic, and lubrication systems. For this purpose, measures to control fuel temperature need to be determined. The primary role of the thermal management for engines is engine cooling, especially the cooling of engine turbine and combustor walls. Supersonic and hypersonic flight vehicles need thermal protection systems to protect the structures from high temperature damage caused by aerodynamic heating. This Special Issue of Aerospace covers recent advances in aerospace thermal management science and technology.

An additional topic of interest in this Special Issue is the advancements in the application of thermofluids, especially heat transfer and fluid dynamics, to aerospace thermal management systems.

Prof. Dr. Xiande Fang
Dr. Zhanru Zhou
Guest Editors

Manuscript Submission Information

Manuscripts should be submitted online at www.mdpi.com by registering and logging in to this website. Once you are registered, click here to go to the submission form. Manuscripts can be submitted until the deadline. All submissions that pass pre-check are peer-reviewed. Accepted papers will be published continuously in the journal (as soon as accepted) and will be listed together on the special issue website. Research articles, review articles as well as short communications are invited. For planned papers, a title and short abstract (about 100 words) can be sent to the Editorial Office for announcement on this website.

Submitted manuscripts should not have been published previously, nor be under consideration for publication elsewhere (except conference proceedings papers). All manuscripts are thoroughly refereed through a single-blind peer-review process. A guide for authors and other relevant information for submission of manuscripts is available on the Instructions for Authors page. Aerospace is an international peer-reviewed open access monthly journal published by MDPI.

Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 2400 CHF (Swiss Francs). Submitted papers should be well formatted and use good English. Authors may use MDPI's English editing service prior to publication or during author revisions.

Keywords

  • aircraft environment control
  • thermal management
  • thermal control
  • avionics cooling
  • life support
  • anti/de-icing
  • turbine cooling
  • heat transfer

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Published Papers

This special issue is now open for submission.
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