UHBR Engine and Ducted Propulsor Noise Reduction Technology for Future Aircraft
A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Aeronautics".
Deadline for manuscript submissions: closed (6 December 2024) | Viewed by 2854
Special Issue Editors
Interests: turbomachinery aeroacoustics; noise prediction; noise control; turbomachinery aerothermal dynamics
Interests: aeroacoustics; bionic noise reduction; noise prediction; propeller noise; noise measurement
Special Issues, Collections and Topics in MDPI journals
Special Issue Information
Dear Colleagues,
Ultra-high bypass ratio (UHBR) engines and ducted propulsors are indispensable power devices for future aircraft. For UHBR engines and ducted propulsors, the forward and afterward radiating fan noise is one of the most important noise sources. Three primary noise sources of the fan are the rotor-stator interaction tonal noise, turbulence broadband noise and shock noise. Advanced noise reduction technology for fans could contribute significantly to future ultra-quiet engines and aircraft. In order to further reveal noise generation mechanisms and reduce noise pollution, it is urgent to conduct systemic research and develop advanced noise reduction technologies for UHBR engines and ducted propulsors.
Potential topics include, but are not limited to:
- The noise characteristics of a ducted fan;
- Fan noise prediction;
- Fan noise reduction;
- The advanced computational aeroacoustics method;
- The advanced computational aerodynamics method;
- The advanced noise measurement method.
Prof. Dr. Weiyang Qiao
Dr. Weijie Chen
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
- UHBR engines
- ducted fan
- aeroacoustics
- noise prediction
- noise reduction
- noise measurement
Benefits of Publishing in a Special Issue
- Ease of navigation: Grouping papers by topic helps scholars navigate broad scope journals more efficiently.
- Greater discoverability: Special Issues support the reach and impact of scientific research. Articles in Special Issues are more discoverable and cited more frequently.
- Expansion of research network: Special Issues facilitate connections among authors, fostering scientific collaborations.
- External promotion: Articles in Special Issues are often promoted through the journal's social media, increasing their visibility.
- e-Book format: Special Issues with more than 10 articles can be published as dedicated e-books, ensuring wide and rapid dissemination.
Further information on MDPI's Special Issue policies can be found here.
