Imperial College Supersonic Wind Tunnel TS4 Equipment 3-c LDA System Dantec Traverse system Micromech

Source URL: www.nwtf.ac.uk

University of Southampton R.J.Mitchell Wind Tunnel LS7 Equipment Tomographic PIV System / Planar Laser Induced Fluorescence System LAVision

Source URL: www.nwtf.ac.uk

Imperial College Hypersonic Gun Tunnel HS1 Location: London Designation: Intermittent impulsive facility

Source URL: www.nwtf.ac.uk

• Aerodynamics
• Numerical control
• Lathe
• G-code
• PLIF
• Reynolds number
• Wind tunnel
• Schlieren
• Fluid dynamics
• Fluid mechanics
• Dynamics

DREAm-TILT Assessment of tiltrotor fuselage drag reduction by wind tunnel tests and CFD State of the art – Background The most recent tiltrotor concepts (such as the future European civil tilt-rotor based on ERICA

Source URL: cleansky.eu

• Aerodynamics
• Fluid dynamics
• Tiltrotor aircraft
• Tiltrotor
• Wind tunnel
• Fixed-wing aircraft
• Drag
• Rotorcraft
• Helicopter
• Aerospace engineering
• Aircraft
• Aviation

PT656 Gurney flap actuator and mechanism for a full scale helicopter rotor blade State of the art – Background Active Gurney Flap (AGF) system that is being developed in PT656 Program takes credit from the

Source URL: www.cleansky.eu

• Aviation
• Gurney flap
• Helicopter
• Wind tunnel
• VTOL aircraft
• Aerospace engineering
• Aircraft
• Helicopter rotor

City University Low Turbulence Wind Tunnel LS1 Equipment 3 component LDV system with traverse Hot wire anemometry system: - Traverse rig and supporting structure

Source URL: www.nwtf.ac.uk

University of Southampton R.J.Mitchell Wind Tunnel LS7 Location: University of Southampton Designation: Low Speed Closed Return

Source URL: www.nwtf.ac.uk

• South East England
• Aerodynamics
• Fluid mechanics
• Wind tunnel
• Sting
• Tunnel
• Southampton
• Local government in England
• Fluid dynamics
• Hampshire

Cambridge University Supersonic Tunnel No. 1&2 TS1, TS2 Location: Cambridge Designation: Transonic/supersonic Open Return blow down

Source URL: www.nwtf.ac.uk

• Fluid mechanics
• Aerospace engineering
• Optics
• Airspeed
• Schlieren
• Mach number
• Shadowgraph
• Transonic speed
• Wind tunnel
• Aerodynamics
• Fluid dynamics
• Dynamics

Glasgow University 9 x 7 Low Speed Wind Tunnel LS5 Equipment 6-component balance, sting and positioning system Data acquisition system

Source URL: www.nwtf.ac.uk

Inflatable Re-entry Vehicle Experiment “A WIND TUNNEL IN THE SKY” NASA’s Inflatable Re-entry Vehicle Experiment, or IRVE, is a mission designed to demonstrate that an inflatable structure can be used as a heat shie

Source URL: www.nasa.gov

• Suborbital spaceflight
• Atmospheric entry
• Space technology
• Black Brant
• Wallops Flight Facility
• Space Shuttle
• Spaceflight
• Transport
• Space