Explore the words cloud of the PERTURB project. It provides you a very rough idea of what is the project "PERTURB" about.
The following table provides information about the project.
AIRCRAFT RESEARCH ASSOCIATION LIMITED
|Coordinator Country||United Kingdom [UK]|
|Total cost||1˙868˙175 €|
|EC max contribution||1˙868˙175 € (100%)|
1. H2020-EU.184.108.40.206. (IADP Regional Aircraft)
|Duration (year-month-day)||from 2019-05-01 to 2021-01-31|
Take a look of project's partnership.
|1||AIRCRAFT RESEARCH ASSOCIATION LIMITED||UK (BEDFORD)||coordinator||1˙689˙570.00|
|2||UNIVERSITY OF BRISTOL||UK (BRISTOL)||participant||178˙605.00|
A CFD characterisation of a regional turboprop configuration with particular focus on the Reynolds number dependence of the power effects, both direct (1P forces and moments) and indirect (slipstream) is performed, in concert with a wind-tunnel test in a pressurised facility to allow variation in Reynolds number. The turboprop is furnished with new control surface concepts. Variable Fidelity Modelling (VFM) techniques are used for the CFD characterisation, deploying steady RANS with actuator disk modelling as the low-fidelity approach and unsteady RANS with full propeller blade modelling as the high-fidelity approach. The latter uses a novel coupling between the RANS solver and a Vortex Particle Method to increase the accuracy of slipstream effects without resorting to costly mesh refinement in the propeller wake. A methodology for determining reliable performance data at full scale is developed, using a combination of CFD and wind-tunnel data at atmospheric conditions only, again deploying VFM.
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The information about "PERTURB" are provided by the European Opendata Portal: CORDIS opendata.
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