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6 European Projects Found

Searched on 125080 European Projects

 FINISHED 
The QB50 Project will demonstrate the possibility of launching a network of 50 CubeSats built by CubeSat teams from all over the world to perform first-class science and in-orbit demonstration in the largely unexplored middle and lower thermosphere. Space agencies are currently not pursuing a multi-spacecraft network for in-situ measurements in the middle and lower thermosphere because the cost of ...
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 17

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... d DBD devices. The Project aims at the improvement of aircraft flight performances.This Project will be carried out in the framework of a EUROPE – RUSSIA cooperation. ONERA is the coordinator, and TSAGI will act as Coordinator of the Russian Partners.There are 12 partners, 7 from Europe and 5 from Russia.ONERA (F), IAG-Stuttgart (G), DLR (G), KTH (S), University of Nottingham (UK), EADS UK Ltd. (U ...
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 13

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... hock waves, which in turn may interact with a laminar boundary layer. Such an interaction can quickly cause flow separation, which is highly detrimental to aircraft performance, and poses a threat to safety. In order to diminish the shock induced separation, the boundary layer at the point of interaction should be turbulent.The main objective of the TFAST project is to study the effect of transiti ...
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RECEPTivity and amplitude-based transition prediction (RECEPT)

Start date: Feb 1, 2011, End date: Apr 30, 2015,

... or technology readiness to reduce fuel consumption and hence emissions. It directly addresses the topic of AAT.2010.1.1.1, AAT.2010.4.1.1 and AAT.2010.4.2.1.The RECEPT consortium consists of 12 organisations from 4 different member states (Sweden, Italy, France Germany) and one of International Cooperation Partner Countries, Russia. It contains 3 aircraft manufacturers (Airbus, SAAB, Piaggio), 5 r ...
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The development of secure and re-usable re-entry vehicle requires the complete control of the heat distribution on its Thermal Protection System (TPS).During the most critical re-entry phase, the hypersonic flow along the vehicle initiates a laminar boundary layer inside of which most of the transfer phenomena take place (heat, momentum and mass transfer). If at one position of the vehicle, this b ...
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 5

 FINISHED 

Technologies for Safe and Controlled Martian Entry (SACOMAR)

Start date: Jan 1, 2011, End date: Jun 30, 2012,

"The main objective of the study is the experimental and numerical study of gas surface interaction phenomena in the high enthalpy flow field behind the bow shock in front of a model at Martian entry flow conditions. The improvement of physical modelling using experimental data and its implementation into the CFD codes is essential to understand and interpret the physical processes. At the end the ...
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