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  • 服务 » Aircraft Research Association
    zh New Page zh New Page zh New Page zh Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Search Sub menu About ARA History Founding Member Companies Timeline of Significant Events Location Contact Information Partnerships People Senior Management Team Retirement Club Charities 服务 实验空气动力学 Transonic Wind Tunnel Testing Civil Aircraft Drag Performance Stability and Control Rear Fuselage Performance Installed Propulsion Performance Isolated Propulsion Performance Military Aircraft UAV s and Missiles Store Separation Stability and Control Intake Performance Installed Store Loads Isolated Store Loads Data Quality and Repeatability Productivity Customer Facilities Other Test Facilities Balance Calibration Laboratory Mach Simulation Tank Propeller Test Cell Small Scale Transonic Tunnel 2 Dimensional Tunnel Large Scale Thrust Measuring Rig New Page zh 设计与制造 CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture 计算流体动力学 CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research 创新与技术 Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement New Page zh Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies New Page zh New Page zh New Page zh

    Original URL path: http://www.ara.co.uk/zh/services/ (2016-02-17)
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  • Transonic Wind Tunnel Testing » Aircraft Research Association
    Isolated Propulsion Performance Military Aircraft UAV s and Missiles Store Separation Stability and Control Intake Performance Installed Store Loads Isolated Store Loads Data Quality and Repeatability Productivity Customer Facilities Other Test Facilities Balance Calibration Laboratory Mach Simulation Tank Propeller Test Cell Small Scale Transonic Tunnel 2 Dimensional Tunnel Large Scale Thrust Measuring Rig New Page fr Conception et Fabrication CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Mécanique des Fluides Numérique CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Innovation et technologie Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement New Page fr Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies New Page fr New Page fr New Page fr New Page fr Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Transonic Wind Tunnel Testing Aircraft Research Association Services Aérodynamique Expérimentale Transonic Wind Tunnel Testing Since 1956 ARA has provided wind tunnel data of the highest quality by developing and utilising highly efficient world class techniques for our global civil and military aerospace customer base The ARA Transonic Wind Tunnel TWT is a closed circuit continuous flow tunnel with the following operational features Test section 2 74m wide x 2 44m high 9ft x 8ft Four porous walls 22 maximum porosity Mach number 0 to 1 4 Stagnation pressure 0 8 to 1 2 atmospheres standard operation is 1 atmosphere Reynolds number 3 5 to 16 7 million m dependent upon Mach number The TWT has a number of support systems for a wide range of test types Rear single sting support basic incidence range 10 to 40 180 roll range High incidence offset

    Original URL path: http://www.ara.co.uk/fr/services/aerodynamique-experimentale/transonic-wind-tunnel-testing/ (2016-02-17)
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  • Transonic Wind Tunnel Testing » Aircraft Research Association
    Isolated Propulsion Performance Military Aircraft UAV s and Missiles Store Separation Stability and Control Intake Performance Installed Store Loads Isolated Store Loads Data Quality and Repeatability Productivity Customer Facilities Other Test Facilities Balance Calibration Laboratory Mach Simulation Tank Propeller Test Cell Small Scale Transonic Tunnel 2 Dimensional Tunnel Large Scale Thrust Measuring Rig New Page es Diseño y fabricación CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Dinámica de fluidos computacional CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Innovación y tecnología Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement New Page es Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies New Page es New Page es New Page es New Page es Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Transonic Wind Tunnel Testing Aircraft Research Association Servicios Aerodinámica experimental Transonic Wind Tunnel Testing Since 1956 ARA has provided wind tunnel data of the highest quality by developing and utilising highly efficient world class techniques for our global civil and military aerospace customer base The ARA Transonic Wind Tunnel TWT is a closed circuit continuous flow tunnel with the following operational features Test section 2 74m wide x 2 44m high 9ft x 8ft Four porous walls 22 maximum porosity Mach number 0 to 1 4 Stagnation pressure 0 8 to 1 2 atmospheres standard operation is 1 atmosphere Reynolds number 3 5 to 16 7 million m dependent upon Mach number The TWT has a number of support systems for a wide range of test types Rear single sting support basic incidence range 10 to 40 180 roll range High incidence offset

    Original URL path: http://www.ara.co.uk/es/servicios/aerodinamica-experimental/transonic-wind-tunnel-testing/ (2016-02-17)
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  • Transonic Wind Tunnel Testing » Aircraft Research Association
    Isolated Propulsion Performance Military Aircraft UAV s and Missiles Store Separation Stability and Control Intake Performance Installed Store Loads Isolated Store Loads Data Quality and Repeatability Productivity Customer Facilities Other Test Facilities Balance Calibration Laboratory Mach Simulation Tank Propeller Test Cell Small Scale Transonic Tunnel 2 Dimensional Tunnel Large Scale Thrust Measuring Rig New Page de Technische Planung und Herstellung CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Numerische Strömungsmechanik CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Innovation und Technik Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement New Page de Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies New Page de New Page de New Page de New Page de Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Transonic Wind Tunnel Testing Aircraft Research Association Dienstleistungen Experimentelle Aerodynamik Transonic Wind Tunnel Testing Since 1956 ARA has provided wind tunnel data of the highest quality by developing and utilising highly efficient world class techniques for our global civil and military aerospace customer base The ARA Transonic Wind Tunnel TWT is a closed circuit continuous flow tunnel with the following operational features Test section 2 74m wide x 2 44m high 9ft x 8ft Four porous walls 22 maximum porosity Mach number 0 to 1 4 Stagnation pressure 0 8 to 1 2 atmospheres standard operation is 1 atmosphere Reynolds number 3 5 to 16 7 million m dependent upon Mach number The TWT has a number of support systems for a wide range of test types Rear single sting support basic incidence range 10 to 40 180 roll range High incidence offset roll

    Original URL path: http://www.ara.co.uk/de/dienstleistungen/new-service-page-de/transonic-wind-tunnel-testing/ (2016-02-17)
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  • Transonic Wind Tunnel Testing » Aircraft Research Association
    Performance Installed Propulsion Performance Isolated Propulsion Performance Military Aircraft UAV s and Missiles Store Separation Stability and Control Intake Performance Installed Store Loads Isolated Store Loads Data Quality and Repeatability Productivity Customer Facilities Other Test Facilities Balance Calibration Laboratory Mach Simulation Tank Propeller Test Cell Small Scale Transonic Tunnel 2 Dimensional Tunnel Large Scale Thrust Measuring Rig New Page zh 设计与制造 CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture 计算流体动力学 CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research 创新与技术 Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement New Page zh Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies New Page zh New Page zh New Page zh New Page zh Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Transonic Wind Tunnel Testing Aircraft Research Association 服务 实验空气动力学 Transonic Wind Tunnel Testing Since 1956 ARA has provided wind tunnel data of the highest quality by developing and utilising highly efficient world class techniques for our global civil and military aerospace customer base The ARA Transonic Wind Tunnel TWT is a closed circuit continuous flow tunnel with the following operational features Test section 2 74m wide x 2 44m high 9ft x 8ft Four porous walls 22 maximum porosity Mach number 0 to 1 4 Stagnation pressure 0 8 to 1 2 atmospheres standard operation is 1 atmosphere Reynolds number 3 5 to 16 7 million m dependent upon Mach number The TWT has a number of support systems for a wide range of test types Rear single sting support basic incidence range 10 to 40 180 roll range High incidence offset roll system up to

    Original URL path: http://www.ara.co.uk/zh/services/page-11/transonic-wind-tunnel-testing/ (2016-02-17)
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  • Conception et Fabrication » Aircraft Research Association
    Military Aircraft UAV s and Missiles Store Separation Stability and Control Intake Performance Installed Store Loads Isolated Store Loads Data Quality and Repeatability Productivity Customer Facilities Other Test Facilities Balance Calibration Laboratory Mach Simulation Tank Propeller Test Cell Small Scale Transonic Tunnel 2 Dimensional Tunnel Large Scale Thrust Measuring Rig New Page fr Conception et Fabrication CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Mécanique des Fluides Numérique CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Innovation et technologie Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement New Page fr Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies New Page fr New Page fr New Page fr New Page fr Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Conception et Fabrication Aircraft Research Association Services Conception et Fabrication Avec une histoire débutant en 1956 le département de conception et de fabrication des maquettes d ARA a une vaste expérience dans la conception et la fabrication de maquettes de souffleries de matériaux spécialisés de test et d équilibre de jauges de contraintes pour les souffleries chez ARA et les agences externes ARA produit des maquettes pour le test en souffleries à faible vitesse transsonique supersonique et hypersonique en Europe en Amérique et en Asie et dans les deux installations cryogéniques les plus grandes du monde la soufflerie transsonique cryogénique européenne ETW en Allemagne et la NASA National Transonic Facility NTF Installation Transsonique Nationale aux États Unis Objectif principal minimiser le temps de cycle entre la maquette définitive du client et la livraison des données de la soufflerie Réputation mondiale pour la production de maquettes de

    Original URL path: http://www.ara.co.uk/fr/services/conception-et-fabrication/ (2016-02-17)
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  • Diseño y fabricación » Aircraft Research Association
    Control Intake Performance Installed Store Loads Isolated Store Loads Data Quality and Repeatability Productivity Customer Facilities Other Test Facilities Balance Calibration Laboratory Mach Simulation Tank Propeller Test Cell Small Scale Transonic Tunnel 2 Dimensional Tunnel Large Scale Thrust Measuring Rig New Page es Diseño y fabricación CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Dinámica de fluidos computacional CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Innovación y tecnología Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement New Page es Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies New Page es New Page es New Page es New Page es Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Diseño y fabricación Aircraft Research Association Servicios Diseño y fabricación Con unos comienzos que datan de 1965 el departamento de diseño y fabricación de modelos de ARA tiene una vasta experiencia en el diseño y fabricación de modelos de túneles de viento instalaciones de pruebas especiales y balanzas extensimétricas para túneles de viento tanto para ARA como para agencias externas ARA fabrica modelos para pruebas en túneles de viento de baja velocidad transónicos supersónicos e hipersónicos en Europa América y Asia También fabrica para las dos mayores instalaciones criogénicas del mundo concretamente para el Túnel de Viento Transónico Europeo European Transonic Wind Tunnel ETW en Alemania y para el Centro Nacional Transónico de la NASA NASA National Transonic Facility NTF en Norteamérica El objetivo principal es reducir el tiempo de ciclo que existe entre la pausa del proceso de diseño y la entrega de los datos del túnel de viento a los clientes Reputación mundial por

    Original URL path: http://www.ara.co.uk/es/servicios/diseno-y-fabricacion/ (2016-02-17)
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  • Experimentelle Aerodynamik » Aircraft Research Association
    Bay Analysis Wing Design Process Aerodynamic Research Innovation und Technik Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement New Page de Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies New Page de New Page de New Page de New Page de Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Experimentelle Aerodynamik Aircraft Research Association Dienstleistungen Experimentelle Aerodynamik Seit der Gründung von ARA im Jahr 1956 liefert die Abteilung Experimentelle Aerodynamik Windkanaldaten höchster Qualität mit denen dann unser internationaler Kundenstamm in den Bereichen der zivilen und der militärischen Luft und Raumfahrt von Amerika bis nach Asien versorgt wird ARA ist bekannt für qualitativ hochwertige Daten eine zugesicherte Wiederholgenauigkeit und ein hohes Maß an Produktivität Wir stellen im Entwicklungszyklus der Flugzeugherstellung ein wichtiges Bindeglied dar und ermöglichen es dabei der Luft und Raumfahrtindustrie gleichzeitig entweder unsere computerbasierte Analyse zu übernehmen und zu ergänzen oder komplexe Strömungen mit einer Geschwindigkeit und Genauigkeit zu untersuchen die selbst über die wohl besten computerbasierten Simulationsmöglichkeiten hinausgeht welche heute in diesem Bereich zur Verfügung stehen Aufbau von starken verlässlichen Beziehungen mit führenden Unternemen der Luft und Raumfahrt Forschungsgemeinschaften und Regierungsorganisationen durch eine Kombination aus unserem Know how und unserem Engagement dahingehend die Bedürfnisse unserer Kunden zu verstehen und entsprechend auf diese reagieren zu können Wir sind stolz darauf dass wir effiziente und flexible Dienstleistungen anbieten können die mit einem ausgezeichneten Preis Leistungs Verhältnis einher gehen Wir bedienen unsere Kunden mit einer breiten Palette an Untersuchungsmöglichkeiten für sowohl die zivile als auch die militärische Luft und Raumfahrt wie z B das Messen von Widerstandskräften beim Bau noch umweltfreundlicherer und noch sparsamerer Flugzeuge oder auch die Überprüfung einer entsprechenden Speichertrennung sog Store Separation bei einem Kampfjet zur Gewährleistung der Sicherheit des Flugzeugs und der Piloten Dank der bei

    Original URL path: http://www.ara.co.uk/de/dienstleistungen/new-service-page-de/ (2016-02-17)
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web-archive-uk.com, 2016-12-05