Adjoint-Based Techniques in Computational Fluid Dynamics: Theory and Applications
A special issue of Aerospace (ISSN 2226-4310).
Deadline for manuscript submissions: 20 December 2025 | Viewed by 377
Special Issue Editors
Interests: aeroelasticity; computational fluid dynamics; aerodynamics; numerical simulation; fluid mechanics; aeronautical engineering; mechanical engineering
Special Issues, Collections and Topics in MDPI journals
Interests: aerodynamics; computational fluid dynamics; adjoint methods
Special Issues, Collections and Topics in MDPI journals
Special Issue Information
Dear Colleagues,
This Special Issue aims to cover ongoing advances in the development and application of adjoint methods in fluid dynamics. In addition to original research articles, review papers, letters or communications, technical reports, and extended versions of conference papers are likewise accepted.
The main topics that we expect to cover include the following:
- Properties of adjoint solutions, including analytic results;
- Continuous, discrete and unsteady adjoint implementations, including new developments concerning robustness, accuracy and time-efficiency of adjoint solvers;
- Shape parameterisation and robust mesh deformation;
- Aplication of adjoint methods to multidisciplinary shape optimization, error estimation and goal-oriented mesh adaptation, uncertainty quantification and robust design, data assimilation, stability analysis, etc.
Dr. Jorge Ponsin
Dr. Carlos Lozano
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
- adjoint equations
- continuous adjoint method
- discrete adjoint method
- aerodynamic design
- properties of adjoint solutions
- gradient-based optimization
- computational fluid dynamics
- multidisciplinary optimization
- adjoint-based stability analysis
- error estimation and mesh adaptation
- uncertainty quantification
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