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4 European Projects Found

Searched on 125080 European Projects

 FINISHED 

Composite fuselage section Wafer Design Approach for Safety Increasing in Worst Case Situations and Joints Minimizing (WASIS)

Start date: Jan 1, 2011, End date: Dec 31, 2014,

"Aeronautics is a key asset for the future of Europe, but nowadays the industry has to face the challenge of “More Affordable, Safer, Cleaner and Quieter” while at the same time accounting for a demand that will triple over the next 20 years. WASIS project aims to rise to this challenge with the development of a composite fuselage structure based on the lattice stiffening concept, optimizing geome ...
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 14

 FINISHED 

Gas Flows in Micro Electro Mechanical Systems (GASMEMS)

Start date: Oct 1, 2008, End date: Sep 30, 2012,

Gas flows in microsystems are of great interest for various applications that touch almost every industrial field. This diversity is typified through the following examples: fluidic microactuators for active control of aerodynamic flows, vacuum generators for extracting biological samples, mass flow and temperature micro-sensors, pressure gauges, micro heat-exchangers for the cooling of electronic ...
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 14

 FINISHED 

HeliconPlasmaHydrazine.COmbinedMicro (HPH.com)

Start date: Dec 1, 2008, End date: May 31, 2012,

The objective of the research program is to design, optimize and develop a space plasma thruster based on helicon-radio-frequency technology and its application to a nano-satellite for attitude and position control. Moreover a detailed feasibility study will be also conducted to evaluate the possibility of using the plasma thruster to heat and decompose a secondary propellant. The feasibility stud ...
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 15

 FINISHED 

Numerical Simulation and Design Optimization of a Lower Fuselage Structure with Advanced Integral Stiffening (FusDesOpt)

Start date: Jan 1, 2010, End date: Jun 30, 2010,

This proposal is for the structural analysis and design optimization of the lower fuselage of an aircraft. The objective of the structural optimization is minimum weight and the design constraints fall into two categories; firstly the capability to withstand structural loads with sufficient margins, and secondly constraints relating to the manufacturing methods. The structure to be optimized is a ...
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