Explore the words cloud of the FURADO project. It provides you a very rough idea of what is the project "FURADO" about.
The following table provides information about the project.
Coordinator |
TECHNISCHE UNIVERSITAET MUENCHEN
Organization address contact info |
Coordinator Country | Germany [DE] |
Project website | http://www.furado.tum.de |
Total cost | 399˙000 € |
EC max contribution | 399˙000 € (100%) |
Programme |
1. H2020-EU.3.4.5.3. (IADP Fast Rotorcraft) |
Code Call | H2020-CS2-CFP01-2014-01 |
Funding Scheme | CS2-IA |
Starting year | 2016 |
Duration (year-month-day) | from 2016-03-01 to 2020-02-29 |
Take a look of project's partnership.
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1 | TECHNISCHE UNIVERSITAET MUENCHEN | DE (MUENCHEN) | coordinator | 399˙000.00 |
The project is aimed on the numerical design optimization and flow analysis of a semi-watertight full fairing rotor head with respect to drag reduction of a compound helicopter configuration, namely the Low Impact, Fast and Efficient Rotorcraft (LifeRCraft) demonstrator. It has been shown that fully fairing the structural components of the rotor head as a whole provides significant drag reduction potential. The project first phase concentrates on the method development for all consecutive steps. This includes enhancing the existing CFD and optimizer software to be able to automatically optimize the fairing geometries. The software functionality is demonstrated by performing computations of the rotor head blade sleeve fairings, the full-fairing beanie and the pylon fairing for a series of simplified flow conditions. The second phase of the project is dedicated to pre-development of potential rotor head full fairing configurations. A special focus is on preliminary optimisations of the blade sleeves, beanie and hub fairing for forward flight conditions with a non-spinning rotor head. The following development phase addresses two tasks. The first task comprises a refined aerodynamic optimization of promising full fairing configurations under the effect of rotor rotation. Flow conditions inside the fairing are also thermically analyzed to avoid any overheating of components. The second task is on wake flow analysis of the drag-reducing full fairing geometries performing high precision aerodynamic simulations. Strong unsteady airloads on the empennage due to the rotor head wake must be avoided to ensure proper flight dynamics and structural integrity. Consequently, the project results in a seamless integration of the developed software tools into the topic leaders work flow. The complex, CPU-intensive CFD simulations establish a sound data base for full fairing rotor head design and analysis which is not available today.
Project webpage accessible to the public | Websites, patent fillings, videos etc. | 2019-05-30 13:57:56 |
Take a look to the deliverables list in detail: detailed list of FURADO deliverables.
year | authors and title | journal | last update |
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2018 |
P. Pölzlbauer, D. Desvigne, C. Breitsamter Performance improvement of a compound helicopter rotor head by aerodynamic shape optimization published pages: , ISSN: , DOI: |
31st Congress of the International Council of the Aeronautical Sciences Every two years | 2019-05-22 |
2019 |
P. Pölzlbauer, C. Breitsamter, D. Desvigne Performance improvement of a compound helicopter rotor head by aerodynamic design optimisation of a blade-sleeve fairing published pages: 1-20, ISSN: 0001-9240, DOI: 10.1017/aer.2018.172 |
The Aeronautical Journal | 2019-05-22 |
2018 |
P. Pölzlbauer, D. Desvigne, C. Breitsamter Aerodynamic design optimization of a helicopter rotor blade-sleeve fairing published pages: , ISSN: 1869-5582, DOI: 10.1007/s13272-018-0341-0 |
CEAS Aeronautical Journal | 2019-05-22 |
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The information about "FURADO" are provided by the European Opendata Portal: CORDIS opendata.