Details
European Transonic Windtunnel (ETW)
                              			

                           Wind tunnels, using scaled down aircraft models, are the major source of aerodynamic design data for new aircraft projects.
                                 Wind tunnels are indispensable tools for aerodynamic research and aircraft development, and complement the most powerful computers.
ETW,
                                 the European Transonic Wind Tunnel, was designed, constructed and is operated by the four European countries France, Germany,
                                 Great Britain and The Netherlands based on a non-profit policy. It is located in Cologne, Germany.
European researchers and
                                 engineers harness ETW’s capabilities for advancing aeronautical science into aircraft innovation by accessing real-flight
                                 conditions in this cutting edge ground-test laboratory. Training opportunities for researchers and engineers are provided.
ETW
                                 is the worldwide leading wind tunnel for testing aircraft at real flight conditions. Aircraft performance and their flight
                                 envelope limits can be accurately determined with unique quality at ETW long before flight testing of a first prototype. This
                                 enables significant reduction in the technical and economic risks associated with the development of new aircraft. Manufacturers
                                 from all over the world take advantage of the exceptional features of this high-tech facility enhancing the performance, economic
                                 viability, and environmental friendliness of their future aircraft.
ETW operation and access complies with ISO9001:2008 quality
                                 management.
                              
                              Address: Ernst-Mach-Strasse
51147 Köln
Nordrhein-Westfalen
Deutschland
To website
                                 51147 Köln
Nordrhein-Westfalen
Deutschland
To website
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                                    Host Institution
Gesellschafter Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)
Linder Höhe
51147 Köln
Nordrhein-Westfalen
Deutschland
Http://www.dlr.de
                                 Linder Höhe
51147 Köln
Nordrhein-Westfalen
Deutschland
Http://www.dlr.de
Gesellschafter Stichting Nationaal Lucht- en Ruimtevaartlaboratorium (NLR)
Anthony Fokkerweg 2
1059 CM Amsterdam
Niederlande
http://www.nlr.nl
                                 Anthony Fokkerweg 2
1059 CM Amsterdam
Niederlande
http://www.nlr.nl
Gesellschafter Department for Business, Energy & Industrial Strategy (BIS)
1 Victoria Street
SW1H 0ET London
England
https://www.gov.uk/government/organisations/department-for-business-energy-and-industrial-strategy
                                 1 Victoria Street
SW1H 0ET London
England
https://www.gov.uk/government/organisations/department-for-business-energy-and-industrial-strategy
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                                    Scientific Domain
Primary Subjects: 
                                       
                                 - Mechanical and Industrial Engineering
Secondary Subjects: 
                                       
                                 - Physics
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                                    Category
Wind Tunnels, Fluid Dynamics
                                 - 
                                    Scientific Services
ETW offers worldwide experimental wind tunnel investigations focussing on aerodynamic and aeroelastic measurements on lifting
                                    bodies in the subsonic, transonic or supersonic speed range up to Mach-numbers of 1.35. Taking the benefit of the cryogenic
                                    technique is allowing for an extremely accurate simulation of  flow effects at high Reynolds-numbers of up to 90 Million.
                                    Beside classic measurements of forces and moments additional techniques are available for analyses of the origination and
                                    development of aerodynamic processes. The application and operation of non intrusive techniques is here the most favoured
                                    approach.
A small cryogenic wind tunnel scaled 1:8.8 is additionally available for basic investigations as well as for the
                                    development or adaptation of new techniques for operation under cryogenic conditions. Further on, a worldwide unique balance
                                    calibration rig covering the full temperature range from ambient down to cryogenics is available for balance calibrations.
                                    Two cryogenic chambers of different size can be offered for investigations of temperature effects  on structural elements
                                    or mechanical components not requiring fluid flow.
                                 
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                                    Scientific Equipment
- Balances for Force -& Moment Measurements
- Pressure Measurement system
- Optical Deformation measurement system
- Transition detection by temp. sensitive paint
- Pressure measurem. by press. sensitive paint
- Flow field analysis with PIV
- Unsteady pressure measurement system
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                                    Keywords
- Aerodynamic
- Aeroelastic
- Wind tunnel measurements
- Wind tunnel measurement technique
- Flight Reynolds-number Simulation
- Cryogenic Temperatures
- Liquid Nitrogen
- Aeroakustik
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                                    Networks
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                                    Users per annum
Internal Users: 4
                                 External Users in total: 
60
                                 External Users: 12
                                 External Users in the EU: 30
                                 External Users outside of EU: 18
                                 

