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Aeronautical Systems for Flow Control
This special issue belongs to the section “Aeronautics“.
Special Issue Information
Dear Colleagues,
The increasing demands placed on air traffic in terms of nitrogen oxide emissions, noise emissions and fuel consumption, while at the same time increasing the volume of air transport, call for completely new technical approaches. In particular, aeronautical systems for flow control promise significantly improved laminarity of the flow, significantly increased high-lift properties with simultaneously reduced noise emission from the flow around profiles.
This Special Issue aims to provide an overview of recent advances in aeronautical systems for flow control and its application to civil aircraft. Authors are invited to submit full research articles and review manuscripts addressing (but not limited to) the following topics:
- Morphing airfoils (control surfaces, winglets, etc.)
- Flow control by boundary layer suction and blow-out
- Active measures to maintain laminar flow
- Adaptive high-lift devices
- Sensing technologies for flow control
- High-lift systems for steep ascent and descent
- Measures to reduce noise emissions from advanced high-lift systems
- Control algorithms for adaptive systems for flow control
- Experimental on lab scale as well as on full scale profiles
- Simulation methods for adaptive systems for flow control
Prof. Dr. Michael Sinapius
Prof. Dr. Rolf Radespiel
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. 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
- Morphing airfoils (control surfaces, winglets, etc.)
- Flow control by boundary layer suction and blow-out
- Active measures to maintain laminar flow
- Adaptive high-lift devices
- Sensing technologies for flow control
- High-lift systems for steep ascent and descent
- Measures to reduce noise emissions from advanced high-lift systems
- Control algorithms for adaptive systems for flow control
- Experimental on lab scale as well as on full scale profiles
- Simulation methods for adaptive systems for flow control
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