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Advanced Propulsion System and Thermal Management Technology II

A special issue of Energies (ISSN 1996-1073). This special issue belongs to the section "J: Thermal Management".

Deadline for manuscript submissions: closed (30 September 2023) | Viewed by 1191

Special Issue Editors

Research Institute of Aerospace Technology, Central South University, Changsha 410012, China
Interests: gas turbine; convective heat transfer; film cooling; transpiration cooling; scramjet; powder fuel; porous media; combustion; PIV; experimental heat transfer
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Guest Editor
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, China
Interests: supersonic flow and combustion
Special Issues, Collections and Topics in MDPI journals

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Guest Editor
Department of Aerospace Science and Technology, Space Engineering University. Beijing 100416, China
Interests: combustion instability and spray dynamics related to gas turbine and liquid rocket engines
Special Issues, Collections and Topics in MDPI journals

Special Issue Information

Dear Colleagues,

Propulsion systems still receive much research attention, especially aircraft engines, rocket engines and scramjets, etc. Some new propulsion systems are proposed that combine two basic propulsion systems, such as RBCC and TBCC, as well as new types of propulsion systems, such as combined space–air–ocean systems and highly integrated power systems, which can allow aircraft to fly safely from areas over land to those over the ocean. Propulsion systems are developed with the features of a wide speed range and long endurance, both for civil aircraft and military applications. Studies of propulsion systems mainly address their overall design, combustion, aerodynamics, internal flow and heat transfer, etc. High efficiency is pursued not only by optimized design but also via the development of suitable materials as well as the usage of powdered fuel.

Along with the development of high-efficiency propulsion systems, thermal management technology is also developed to address the increased heat from external aerodynamic heating and internal combustion heat at high speeds. This thermal management technology can transfer excessive heat to other low-temperature regions or provide thermal protection for structures via blade cooling in gas turbines and regenerative cooling in rocket engines. The thermal protection of engines is highly efficient due to the enhancement of convective heat transfer, such as the usage of superficial fluids, nanofluids, or newly designed roughened surfaces. Additionally, some heat transfer enhancement methods in heat exchangers, batteries and fuel cells are implemented in propulsion systems.

This Special Issue focuses on bringing together innovative developments in the fields of advanced propulsion systems and thermal management technology. Potential topics include, but are not limited to:

  • Propulsion system design;
  • Heat transfer enhancement;
  • Turbulent combustion;
  • Supercritical fluid;
  • Regenerative cooling;
  • Flow control;
  • Laser-based combustion diagnostics;
  • Spray dynamics;
  • Nanofluids;
  • Blade cooling;
  • Film cooling;
  • Transpiration cooling;
  • Multiphase flow;
  • Heat transfer in propulsion system;
  • Aerodynamics;
  • Combustion instability;
  • Powder fuel;
  • Spray dynamics;
  • Convective heat transfer;
  • Supersonic vehicles;
  • Thermal management in other fields.

Dr. Jian Liu
Prof. Dr. Bengt Sunden
Dr. Chaoyang Liu
Dr. Yiheng Tong
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. Energies is an international peer-reviewed open access semimonthly 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 2600 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

  • propulsion system
  • supersonic vehicles
  • heat transfer
  • combustion
  • turbulence flow
  • thermal protection
  • atomization
  • thermal acoustics
  • spray self-pulsation

Published Papers (1 paper)

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Research

14 pages, 2868 KiB  
Article
Study on the Transformation of Combustion Mechanism and Ejection Phenomenon of Aluminum Particles in Methane Flame
by Sicong Xi, Hongyan Li, Kai Ma, Yingying Lu and Wenxiong Xi
Energies 2023, 16(10), 4057; https://doi.org/10.3390/en16104057 - 12 May 2023
Viewed by 790
Abstract
In solid propellants, the combustion of aluminum particles often occurs in a hydrocarbon combustion atmosphere. In order to study the combustion energy release process of aluminum particles during propellant combustion, we carried out a study of the combustion behavior of aluminum particles in [...] Read more.
In solid propellants, the combustion of aluminum particles often occurs in a hydrocarbon combustion atmosphere. In order to study the combustion energy release process of aluminum particles during propellant combustion, we carried out a study of the combustion behavior of aluminum particles in the combustion atmosphere of hydrocarbon fuels and conducted experiments using a plane flame burner to observe the combustion process of aluminum particles in a methane plane flame combustion atmosphere. High-speed microscopy revealed a new special combustion phenomenon: ejection combustion with the release of internal components from a point on the particle at high speed, in addition to the already observed particle microexplosions. Both phenomena show faster-than-normal combustion with short combustion energy release times. The experiments also showed that the combustion behavior of aluminum particles changes with the combustion environment. As the ambient effective oxidizer mole fraction increases from 13% to 29%, the basic combustion behavior of aluminum particles changes from vapor evaporation combustion to multiphase surface combustion. In addition, the percentage of aluminum particles burned by ejection increases from 18.2% to 49.2%, which becomes the dominant mechanism in the special combustion phenomenon of aluminum particles. This paper argues that the multiphase surface combustion provides higher heating rates due to the heat production collected on the particles and the diffusion combustion in the air around the aluminum particles, compared with the evaporation combustion. Therefore, the rate of temperature rise within the particle is affected by the ambient oxidant concentration, leading to a transformation from microexplosion to ejection combustion. The effect of the temperature of the combustion environment on this phenomenon has also been investigated through experiments conducted under different conditions. Full article
(This article belongs to the Special Issue Advanced Propulsion System and Thermal Management Technology II)
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