Aerostructural Analysis, Design, and Optimization
A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Aeronautics".
Deadline for manuscript submissions: closed (31 December 2023) | Viewed by 1937
Special Issue Editors
Interests: structural optimization; composite structure optimization; optimal sensor placement; health monitoring of composites
Special Issues, Collections and Topics in MDPI journals
Special Issue Information
Dear Colleagues,
Simultaneous aerodynamic and structural optimization can significantly improve the overall performance of aerospace vehicles in the design stage. Because of the coupling between aerodynamic and structural disciplines, high-fidelity analysis models are always required in the optimization process. Taking design variables from both disciplines into account, such as aerodynamic geometry, structural layout, and cross-sectional sizes, global optimization methods are demanded to deal with large-scale variables in the optimization problem. Further, with discrete variables originating from manufacturing limitations introduced into the design procedure, efficient optimization techniques are needed to address mixed discrete and continuous variables. Accordingly, aerostructural optimization calls for high-fidelity analysis models and global and efficient optimization methods.
The Special Issue aims to present recent advanced models and methods on aero-structure analysis, design, and optimization, in order to develop applications in drag minimization, weight minimization, and structural safety. The topics of interest for the Special Issue include, but are not limited to:
- High-fidelity and/or multi-fidelity aerostructural analysis model;
- Geometric parameterization in aerostructural analysis;
- Aerostructural coupling analysis method;
- Sensitivity analysis for aerostructural optimization;
- Global and efficient optimization method for aerostructural design;
- Machine learning in aerostructural optimization;
- Aerostructural optimization under uncertainty;
- Geometry, layout, and sizing optimization in aerostructural design;
- Aerostructural optimization with composite structures;
- Flow-induced vibration control of aircraft;
- Fluid–structure interaction (FSI) analysis.
Dr. Haichao An
Dr. Baoshou Zhang
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
- aerodynamic analysis
- aerodynamic design
- structural design
- global and efficient optimization
- sensitivity analysis
- machine learning
