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Large-Eddy Simulation Applications of Combustion Systems

This special issue belongs to the section “Aeronautics“.

Special Issue Information

Dear Colleagues,

Since its very beginning, the aerospace sector has consistently promoted scientific research. In particular, combustion systems, which encompass most aerospace engines for thrust generation, have been driving investigations into thermofluid dynamics, with a positive impact on other sectors, too, such as power generation for electric systems. The great interest in burning green propellants in gas turbines has opened new challenges for the identification of the most suitable combustion technology. The renewed interest in access to space adopting reusable launchers is pushing research in liquid and air-breathing rocket engines. Further, chemical propulsion has a main role in hypersonic and supersonic vehicles for atmospheric and trans-atmospheric flights and in missile interception. In such applications, the dynamics of reacting flows plays a central role. Although not yet fully integrated in the design process at industrial level due to its longer time-to-solution with respect to the commonly adopted RANS/FANS approach, large eddy simulation, able to capture large (resolved) turbulent scales behavior, is of great help in investigating dynamic physical mechanisms and in looking for control strategies to develop innovative combustion systems.

This Special Issue of Aerospace focuses on articles dealing with LES numerical investigation of combustion systems for gas turbines, ramjet, scramjet, liquid, solid, and hybrid rocket engines, especially covering topics where the role of dynamics is crucial, such as thermoacoustic instabilities, flame stabilization, blow-off, and real gas effects.

Dr. Eugenio Giacomazzi
Guest Editor

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 250 words) can be sent to the Editorial Office for assessment.

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

  • combustion
  • thermo-acoustics
  • flame stabilization
  • flame blow-off
  • mixing
  • real gas
  • high-pressure
  • trans-critical injection
  • supercritical flow
  • radiative energy transfer
  • gas turbine
  • ramjet
  • scramjet
  • rocket

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Aerospace - ISSN 2226-4310