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  • Mach Simulation Tank » Aircraft Research Association
    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 Mach Simulation Tank Aircraft Research Association Servicios Aerodinámica experimental Other Test Facilities Mach Simulation Tank The Mach Simulation Tank MST is used for mass flow and thrust drag calibration of through flow nacelles TFN turbine powered simulator TPS nacelles ducted models and nozzle systems This facility is used to support propulsion testing in the Transonic Wind Tunnel TWT but is also

    Original URL path: http://www.ara.co.uk/es/servicios/aerodinamica-experimental/other-test-facilities/mach-simulation-tank/ (2016-02-17)
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  • Propeller Test Cell » Aircraft Research Association
    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 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 Propeller Test Cell Aircraft Research Association Servicios Aerodinámica experimental Other Test Facilities Propeller Test Cell The propeller test cell is used for model assembly systems installation and

    Original URL path: http://www.ara.co.uk/es/servicios/aerodinamica-experimental/other-test-facilities/propeller-test-cell/ (2016-02-17)
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  • 2-Dimensional Tunnel » Aircraft Research Association
    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 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 2 Dimensional Tunnel Aircraft Research Association Servicios Aerodinámica experimental Other Test Facilities 2 Dimensional Tunnel The two dimensional wind tunnel is used to test aerofoil sections at speeds between Mach 0 3 and 0 87 The tunnel test section is 0 2m 8in by 0 46m 18in The typical model chord length is 0 127m 5in The maximum unit Reynolds number is 55 million per metre The stagnation pressure ranges between 1 5 and 4 0 bars atmospheric pressure The incidence range for models is 11 to 20 The 2 Dimensional tunnel is mainly used for dynamic testing and analysis of helicopter rotor blade section performance The model is mounted in the Enhancing Rate Pitching System ERPS which is used to simulate the rotor blade dynamics to assess dynamic stall of the retreating

    Original URL path: http://www.ara.co.uk/es/servicios/aerodinamica-experimental/other-test-facilities/2-dimensional-tunnel/ (2016-02-17)
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  • Large Scale Thrust Measuring Rig » Aircraft Research Association
    experimental 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 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 Large Scale Thrust Measuring Rig Aircraft Research Association Servicios Aerodinámica experimental Other Test Facilities Large Scale Thrust Measuring Rig The Large Scale Thrust Measuring Rig LSTMR is used for testing twin stream and single stream nozzle systems including twin stream mixers and thrust reversers This testing facility has been relocated to S C Thermofluids Ltd Photograph courtesy of S C Thermofluids Ltd Facility Capabilities ISO 9300 metered mass flows of up to 12kg s 26 5Ibs sec fan and 7kg s 15 4Ibs sec core Cold or hot core up to 600 C 1112 F using a hydrogen burner Total Pressure ratios of up to 5 1 fan and 4 1 core 8 900N 2 000lbf axial thrust capacity with lateral force measurement capability for

    Original URL path: http://www.ara.co.uk/es/servicios/aerodinamica-experimental/other-test-facilities/large-scale-thrust-measuring-rig/ (2016-02-17)
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  • CAD Design Services » Aircraft Research Association
    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 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 CAD Design Services Aircraft Research Association Servicios Diseño y fabricación CAD Design Services The Design Office has over 50 years experience in the design of wind tunnel models and related equipment The office has a combined experience of over 80 years covering a wide range of model types and rigs both for conventional and cryogenic wind tunnels worldwide These include Complete and half models Civil and military models Icing models Helicopter models Low speed models Turbofan propeller simulation systems Engine intake exhaust rigs Aircraft stores A wide range of force measuring balances main model store rotary control surface Wind Tunnel hardware and other specialist rigs In the past ARA has frequently been required to provide turnkey projects for Customers resulting in the model design being tested in ARAs large Transonic Wind Tunnel Consequently a design culture has evolved and developed that

    Original URL path: http://www.ara.co.uk/es/servicios/diseno-y-fabricacion/cad-design-services/ (2016-02-17)
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  • Inspection Services » Aircraft Research Association
    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 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 Inspection Services Aircraft Research Association Servicios Diseño y fabricación Inspection Services Measurement using Renishaw SP25 Analogue Scanning Probe Up to 1000 data points measured per second

    Original URL path: http://www.ara.co.uk/es/servicios/diseno-y-fabricacion/inspection-services/ (2016-02-17)
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  • Finite Element Analysis » Aircraft Research Association
    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 Finite Element Analysis Aircraft Research Association Servicios Diseño y fabricación Finite Element Analysis Whether a model design is being tested at ARA or another facility is irrelevant all test hardware will be subject to meeting specific strength and safety requirements To support the design process and preliminary hand calculations

    Original URL path: http://www.ara.co.uk/es/servicios/diseno-y-fabricacion/finite-element-analysis/ (2016-02-17)
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  • Applied Aerodynamics » 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 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 Applied Aerodynamics Aircraft Research Association Servicios Dinámica de fluidos computacional Applied Aerodynamics ARA has a long history in applying aerodynamic prediction techniques computational and other theoretical to a range of military and civil applications Our strength in aerodynamics has made us the chosen partner of our customers to provide valued support to their in house design and performance assessment teams For several of our customers this degree of joint working has extended over many years Close working with the in house development team enables us to make technological advances and accelerate the adoption of new schemes into our CFD tools where necessary Configurations addressed recently include Civil Aircraft cruise and high lift Open rotors isolated and installed Manned and unmanned military aircraft Weapons isolated and installed Landing gears Formula One cars and other automotive applications The Computational Aerodynamics Applied team offers a wide range of skills

    Original URL path: http://www.ara.co.uk/es/servicios/dinamica-de-fluidos-computacional/applied-aerodynamics/ (2016-02-17)
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