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Transition Location Effect on Shock Wave Boundary Layer Interaction
ID: 265455
Start date: 2012-02-01, End date: 2016-01-31
Vision-2020, whose objectives include the reduction of emissions and a more effective transport systems, puts severe demands on aircraft velocity and weight. These require an increased load on wings and aero-engine components. The greening of air transport systems means a red...
Programme: FP7-TRANSPORT
Record Number: 101445
Last updated on: 2017-05-29
ID: INTAS 2005-1000008-8144
Start date: 2006-09-01, End date: 2009-02-28
Main objective: The main objective of the project is to advance the state-of-the-art in proving and checking techniques for information systems, and to apply them to concrete industrial problems. In more detail, by using practical problems for testing the different methods for...
Programme: IC-INTAS
Record Number: 86127
Last updated on: 2017-03-16
ID: INTAS 2005-1000008-7979
Start date: 2006-10-01, End date: 2009-03-31
Micromechanical behavior of damaged composites subjected to dynamic loading will be investigated. For this purpose, a novel efficient analytical-numerical tool based on the boundary integral equation method (BIEM) or the boundary element method (BEM) will be developed and appl...
Programme: IC-INTAS
Record Number: 86098
Last updated on: 2017-03-16
[PROJECT] INTAS 2005-1000008-7865 - Current topics in string theory
ID: INTAS 2005-1000008-7865
Start date: 2006-11-01, End date: 2008-10-31
Twenty years have passed since string theory has emerged as a viable candidate in search of a unified theory of elementary particles and their interactions; string theory reconciles general relativity with quantum mechanics and contains the main ingredients of the Standard Mod...
Programme: IC-INTAS
Record Number: 86078
Last updated on: 2017-03-16
ID: INTAS 2005-1000008-8046
Start date: 2006-10-01, End date: 2009-03-31
Title: The role of turbulence and electric fields in the formation of transport barriers and the establishment of improved confinement in tokamak plasmas through intermachine comparisons. Over the past decade new regimes of tokamak operation have been identified, whereby elect...
Programme: IC-INTAS
Record Number: 86027
Last updated on: 2017-03-16
ID: INTAS 2005-1000005-7665
Start date: 2006-06-01, End date: 2008-05-31
The principal objective of the present proposal is to develop new types of absorption materials for high-density (gravimetric and volumetric) storage of hydrogen. The subject of the proposal covers the materials synthesis aimed at achieving their improved performance as hydrog...
Programme: IC-INTAS
Record Number: 86026
Last updated on: 2017-03-16
ID: INTAS 2004-79-7165
Start date: 2005-10-01, End date: 2007-09-30
The Enlargement of the EU in 2004 lead to the incorporation of 10 new member states, 8 of them bordering NIS countries. This has created a new borderland between East and West with new kinds of flows of good, people and capital across the borders and especially within the bord...
Programme: IC-INTAS
Record Number: 86012
Last updated on: 2017-03-16
Aircraft external noise research Network and co-ordination
ID: 30840
Start date: 2006-06-01, End date: 2010-11-30
The X3-NOISE Coordination Action, through its network structure and comprehensive workplan involving experts groups, scientific workshops, stakeholders seminars and a common information system, will address the aircraft noise challenges set by the ACARE 20 20 Vision. To thi...
Programme: FP6-AEROSPACE
Record Number: 81470
Last updated on: 2012-10-30
Advanced low cost aircraft structures
ID: 516092
Start date: 2005-02-01, End date: 2011-04-30
The objective is to reduce the operating costs of relevant European aerospace products by 15%, through the cost effective application of carbon fibre composites to aircraft primary structure, taking into account systems integration. The project will seek to reduce aircraft ope...
Programme: FP6-AEROSPACE
Record Number: 75777
Last updated on: 2012-10-19
Multifunctional Structures
[PROJECT] MULFUN - Multifunctional Structures
ID: 516089
Start date: 2005-01-01, End date: 2008-02-29
The needs to reduce cost and provide added value by integration of functions is demanding for a weight and volume constrained design onaircraft and satellite. On the last years, lightweight composite materials have been increasingly used to reduce the structural weight andvolu...
Programme: FP6-AEROSPACE
Record Number: 72841
Last updated on: 2010-10-25
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List retrieved on: 2017-11-25
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