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Subsonic Wind Tunnel

Subsonic Wind Tunnel

50000.00 - 500000.00 INR/Pack

Product Details:


Price And Quantity

  • 1 Pack
  • 50000.00 - 500000.00 INR/Pack

Trade Information

  • 10 Pack Per Month
  • 10-30 Days

Product Description

The Subsonic Wind Tunnel propels you into a realm of innovation and exploration. Whether you're deciphering aerodynamic intricacies, optimizing design parameters, or nurturing the engineers of tomorrow, this facility is your gateway to unlocking the secrets of fluid dynamics. Industries rely on accurate aerodynamic data for design validation and testing. The subsonic wind tunnel offers a controlled environment to validate computational models, assess prototypes, and enhance product quality. For automotive engineers, the wind tunnel provides a platform to enhance vehicle efficiency. Explore drag reduction, lift enhancement, and other aerodynamic improvements, contributing to fuel economy and driving dynamics.


  1. Saves time and money compared to full-scale wind-tunnels or airborne laboratories
  2. Operates at meaningful Reynolds numbers
  3. Compact, open-circuit suction design
  4. Wide variety of experiments in aerodynamics
  5. Comprehensive selection of optional instrumentation, models and ancillaries
  6. High levels of safety
  7. Controls and instrumentation conveniently mount on a separate, free standing frame


  1. A wide variety of subsonic aerodynamics experiments (some need ancillaries), including:
  2. Flow past bluff and streamlined bodies with pressure and velocity observations in the wake
  3. Investigations into boundary layer development
  4. Influence of aspect ratio on aerofoil performance
  5. Performance of an aerofoil with flap, influence of flap angle on lift, drag and stall
  6. Pressure distribution around a cylinder under sub and super-critical flow conditions
  7. Study of characteristics of models involving basic measurement of lift and drag forces
  8. Study of the characteristics of three-dimensional aero foils involving measurement of lift, drag and pitching moment
  9. Study of the pressure distribution around an aerofoil model to derive the lift and comparison with direct measurements of lift.
  10. Drag force on a bluff body normal to an air flow

Available Other :-Subsonic Wind Tunnel

  1. Supersonic Wind Tunnel (Intermittent)

  2. Supersonic Wind Tunnel (Continuous)

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