web-archive-uk.com


Web directory, archive
Search web-archive-uk.com:


Find domain in archive system:
web-archive-uk.com » UK » A » ARA.CO.UK

Total: 524

Choose link from "Titles, links and description words view":

Or switch to "Titles and links view".
  • Mach Simulation Tank » Aircraft Research Association
    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 Optical Systems Design Manufacture CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Computational Aerodynamics CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Research Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement DiPaRT Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies CNC SETTER OPERATOR CNC PROGRAMMER SETTER OPERATOR PROJECT MANAGER PRINCIPAL PROGRAMME MANAGER Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Mach Simulation Tank Aircraft Research Association Services Experimental Aerodynamics 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 available for stand alone

    Original URL path: http://www.ara.co.uk/services/experimental-aerodynamics/other-test-facilities/mach-simulation-tank/ (2016-02-17)
    Open archived version from archive


  • Propeller Test Cell » Aircraft Research Association
    Services Experimental Aerodynamics 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 Optical Systems Design Manufacture CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Computational Aerodynamics CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Research Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement DiPaRT Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies CNC SETTER OPERATOR CNC PROGRAMMER SETTER OPERATOR PROJECT MANAGER PRINCIPAL PROGRAMME MANAGER Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Propeller Test Cell Aircraft Research Association Services Experimental Aerodynamics Other Test Facilities Propeller Test Cell The propeller test cell is used for model assembly systems installation and initial dynamics trial runs

    Original URL path: http://www.ara.co.uk/services/experimental-aerodynamics/other-test-facilities/propeller-test-cell/ (2016-02-17)
    Open archived version from archive

  • Small Scale Transonic Tunnel » Aircraft Research Association
    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 Optical Systems Design Manufacture CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Computational Aerodynamics CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Research Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement DiPaRT Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies CNC SETTER OPERATOR CNC PROGRAMMER SETTER OPERATOR PROJECT MANAGER PRINCIPAL PROGRAMME MANAGER Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Small Scale Transonic Tunnel Aircraft Research Association Services Experimental Aerodynamics Other Test Facilities Small Scale Transonic Tunnel The small scale transonic tunnel is a 1 12 scale version of the Transonic Wind Tunnel TWT This facility is used for low cost wind tunnel testing on small models in the early development stages of a new program It is also used for the calibration of flow angularity meters

    Original URL path: http://www.ara.co.uk/services/experimental-aerodynamics/other-test-facilities/small-scale-transonic-tunnel/ (2016-02-17)
    Open archived version from archive


  • 2-Dimensional Tunnel » Aircraft Research Association
    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 Optical Systems Design Manufacture CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Computational Aerodynamics CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Research Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement DiPaRT Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies CNC SETTER OPERATOR CNC PROGRAMMER SETTER OPERATOR PROJECT MANAGER PRINCIPAL PROGRAMME MANAGER Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact 2 Dimensional Tunnel Aircraft Research Association Services Experimental Aerodynamics 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 blade and shock

    Original URL path: http://www.ara.co.uk/services/experimental-aerodynamics/other-test-facilities/2-dimensional-tunnel/ (2016-02-17)
    Open archived version from archive

  • Large Scale Thrust Measuring Rig » Aircraft Research Association
    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 Optical Systems Design Manufacture CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Computational Aerodynamics CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Research Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement DiPaRT Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies CNC SETTER OPERATOR CNC PROGRAMMER SETTER OPERATOR PROJECT MANAGER PRINCIPAL PROGRAMME MANAGER Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Large Scale Thrust Measuring Rig Aircraft Research Association Services Experimental Aerodynamics 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

    Original URL path: http://www.ara.co.uk/services/experimental-aerodynamics/other-test-facilities/large-scale-thrust-measuring-rig/ (2016-02-17)
    Open archived version from archive

  • Optical Systems » 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 Optical Systems Design Manufacture CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Computational Aerodynamics CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Research Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement DiPaRT Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies CNC SETTER OPERATOR CNC PROGRAMMER SETTER OPERATOR PROJECT MANAGER PRINCIPAL PROGRAMME MANAGER Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Optical Systems Aircraft Research Association Services Experimental Aerodynamics Optical Systems ARA utilises several different types of optical systems for visualisation and measuement of aerodynamic phenomena within it s facilities Many of these have been customised to suit the particular challenges of capturing data within an industrial wind tunnel As these are developed into production systems ARA makes them available to other companies for use in their facilities offering the full design sales installation and support services for these systems A significant area of development in recent years has been around the pressure sensitive paint technologies and techniques and as a result of this ARA has teamed with the US based research and development company ISSI Innovative Scientific Solutions Inc Since 2009 ARA has been the sole European agent and distributor for the ISSI range of products as well as an experienced user within the ARA facilities For further information

    Original URL path: http://www.ara.co.uk/services/experimental-aerodynamics/optical-systems/ (2016-02-17)
    Open archived version from archive

  • CAD Design Services » Aircraft Research Association
    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 Optical Systems Design Manufacture CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Computational Aerodynamics CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Research Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement DiPaRT Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies CNC SETTER OPERATOR CNC PROGRAMMER SETTER OPERATOR PROJECT MANAGER PRINCIPAL PROGRAMME MANAGER Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact CAD Design Services Aircraft Research Association Services Design Manufacture 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 is sympathetic to the needs

    Original URL path: http://www.ara.co.uk/services/design-and-manufacture/cad-design-services/ (2016-02-17)
    Open archived version from archive

  • Inspection Services » Aircraft Research Association
    Charities Services Experimental Aerodynamics 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 Optical Systems Design Manufacture CAD Design Services Precision Model Manufacture Inspection Services Finite Element Analysis Strain Gauge Balance Design and Manufacture Computational Aerodynamics CFD Software Code Development CFD Software Code Application Applied Aerodynamics Integrated CFD Wind Tunnel Weapons and Weapon Bay Analysis Wing Design Process Aerodynamic Research Research Clean Sky Project Strain Gauge Balance Developments Pressure Sensitive Paint Model Deformation Measurement DiPaRT Media Centre Image Library Video Gallery Document Downloads Newsletter Registration Careers Vacancies CNC SETTER OPERATOR CNC PROGRAMMER SETTER OPERATOR PROJECT MANAGER PRINCIPAL PROGRAMME MANAGER Benefits Apprentices Personal Experiences Graduates Industrial Placements Work Experience Contact Inspection Services Aircraft Research Association Services Design Manufacture Inspection Services Measurement using Renishaw SP25 Analogue Scanning Probe Up to 1000 data points measured per second Accuracy volumetric 0 002 Temperature

    Original URL path: http://www.ara.co.uk/services/design-and-manufacture/inspection-services/ (2016-02-17)
    Open archived version from archive



  •  


web-archive-uk.com, 2017-12-11