Explore the words cloud of the STAR project. It provides you a very rough idea of what is the project "STAR" about.
The following table provides information about the project.
Coordinator |
IMPERIAL COLLEGE OF SCIENCE TECHNOLOGY AND MEDICINE
Organization address contact info |
Coordinator Country | United Kingdom [UK] |
Project website | http://www.imperial.ac.uk/mathematics/ |
Total cost | 195˙454 € |
EC max contribution | 195˙454 € (100%) |
Programme |
1. H2020-EU.1.3.2. (Nurturing excellence by means of cross-border and cross-sector mobility) |
Code Call | H2020-MSCA-IF-2014 |
Funding Scheme | MSCA-IF-EF-ST |
Starting year | 2016 |
Duration (year-month-day) | from 2016-01-31 to 2018-01-30 |
Take a look of project's partnership.
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1 | IMPERIAL COLLEGE OF SCIENCE TECHNOLOGY AND MEDICINE | UK (LONDON) | coordinator | 195˙454.00 |
Trailing-edge flows arise in many technological applications, such as aircraft wings in aeronautics and mixing devices in chemical engineering. Two important and fundamental processes take place near the trailing edge, namely the acoustic radiation and receptivity, which refer to generation of sound by fluctuations within the flows and excitations of instability waves by ambient disturbances, respectively. This project will investigate (a) generation of instability waves in the wake as free-stream acoustic and vortical disturbances impinge on the trailing edge; (b) radiation of sound when Tollmien-Schlichting (T-S) waves in the upstream boundary layer propagate through and interact with the trailing-edge flow. Both processes will be analysed mathematically by developing a Local Scattering Theory, which we recently proposed as an appropriate framework for describing the coupling of distinct characteristic motions in a region of strong inhomogenuity. Furthermore, with radiation and receptivity being described properly, we will move on to investigate the so-called acoustic feedback loops, in which instability waves and acoustic waves are generated from each other, leading to self-sustained oscillations. First-principle theories will be developed to predict the intensities as well as the tones (frequencies) of the oscillations. As receptivity, acoustic radiation and acoustic feedback loops are fundamental processes closely related to drag on the wing, jet and airframe noise and mixing of reactants, the present project is of high practical relevance. From the methodology point of view, this project will combine sophisticated asymptotic methods with highly accurate numerical computations, enabling us to tackle a greater range of complex problems, for which numerical or analytical method alone would be inadequate.
year | authors and title | journal | last update |
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2018 |
Ming Dong, Xuesong Wu Generation of symmetric instability modes in the wake behind the trailing edge of a flat plate. Part 2. Transmission of Tollmien-Schlitching wave published pages: , ISSN: 0022-1120, DOI: |
Journal of Fluid Mechanics In preparing | 2019-06-18 |
2018 |
Ming Dong, Xuesong Wu Generation of symmetric instability modes in the wake flow behind the trailing edge of a flat plate. Part 1: receptivity to free-stream sound wave published pages: , ISSN: 0022-1120, DOI: |
Journal Fluid Mechanics Submitted | 2019-06-18 |
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