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Aircraft Aerodynamic Design and Analysis

A special issue of Applied Sciences (ISSN 2076-3417). This special issue belongs to the section "Aerospace Science and Engineering".

Deadline for manuscript submissions: 20 January 2027 | Viewed by 52

Special Issue Editors


E-Mail Website
Guest Editor
CIRA Italian Research Aerospace Centre—Via Maiorise SNC, 81043 Capua, Italy
Interests: fluid mechanics; CFD; shape design; drag breakdown; farfield methods

E-Mail Website
Guest Editor
CIRA Italian Research Aerospace Centre—Via Maiorise SNC, 81043 Capua, Italy
Interests: multi-disciplinary optimisation; machine learning

Special Issue Information

Dear Colleagues,

Aerodynamic challenges in modern aircraft design are continuously growing, due to the increasing demand for a greener aviation and, at the same time, for improved performance competitiveness of the next generation fleet. New, often disruptive, configurations are emerging and, alongside, traditional ones are also being reshaped, introducing, for example, smart trailing edges with morphing movables, active or passive flow control devices, highly integrated distributed power-plant systems, advanced laminar flow solutions and/or surface riblets.

A predictive capability, at multi-fidelity levels, on the aerodynamic force experienced during the different flight phases is therefore of paramount importance, combined with shape optimisation approaches and often integrated in multi-disciplinary frameworks. Digital design tools can nowadays exploit cutting-edge high-performance computing infrastructures, with unsteady analyses of moving parts and/or scale-resolving flow simulations now becoming affordable at design refinement stages. Furthermore, force decomposition methods, including thrust/drag bookkeeping techniques, are increasingly being introduced in aerodynamic analyses, bringing breakdown information to fine-tune design objective functions.

This Special Issue will therefore address, although not being restricted to, the following main topics:

  • Multi-fidelity aerodynamic shape design optimisation.
  • Drag reduction in aeronautics (focusing on induced, viscous and/or wave contributions).
  • Flow control and shape-varying solutions to improve aircraft performance.
  • Advanced machine learning approaches in aircraft design loops.

Research articles proposing original and innovative work are encouraged, but review papers or comparative studies are also welcome.

Dr. Mauro Minervino
Dr. Domenico Quagliarella
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 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. Applied Sciences 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 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

  • aerodynamics
  • CFD
  • shape optimisation
  • drag
  • drag decomposition

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Published Papers

This special issue is now open for submission.
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