Subsonic wind tunnel and accessories

Order Code: 21224953.2.56

Category: General Lab Equipment II

Supersonic Wind Tunnel is a test bed for examining the fluid mechanics and associated fluid phenomena for air travelling faster than the speed of sound. The supersonic wind tunnel is open type wind tunnel working continuously; a variable speed fan i



SPECIFICATION

Specifications:-

  • Velocity Range: Subsonic through Mach 1.8 with help of interchangeable Test Section.

  • Continuous Operation using Variable Speed Air Blower, working on Vacuum Principle.

  • Compressed air collecting tank & air dryer not required (Compared to Intermittent Type Supersonic Wind Tunnel).

  • Schlieren Apparatus with accessories for visualization of Flow at supersonic velocities.

  • Data Acquisition System for measurement & analysis of test parameters

  • Different test models available for study of flow patterns.

Supersonic Wind Tunnel is a test bed for examining the fluid mechanics and associated fluid phenomena for air travelling faster than the speed of sound. The supersonic wind tunnel is open type wind tunnel working continuously; a variable speed fan is used to draw through the wind tunnel. It draws air from the atmosphere & is after flowing through the wind tunne the air is discharged back to the atmosphere. In order to increase the speed of air to supersonic conditions, the air is accelerated through a converging-diverging nozzle. In the measurement section, the air is accelerated further and flows around a drag .The air the flows through the diffuser where it is decelerated before entering the air blower. Interchangeable test sections are provided to generate different velocities. The trainer supplied with four different test models (Wedge, Double wedge, Rocket, Bullet) For observation of the supersonic flow and the resulting shock fronts, the Schlieren optics system is supplied. Pressure sensors are used to measure pressure distribution, & transmitted directly to a computer using a USB based Data Acquisition System for analysis using the software.

Type: Continuous Operating, Induced Flow Supersonic Wind Tunnel

  • Blower:
  • Positive displacement blower
  • Variable Frequency Drive for control of Blower speed
  • Silencer for noise reduction

Test models:

  • Wedge
  • - Double wedge
  • Rocket
  • Bullet

(Other Test Models available on request)

Schlieren Apparatus: Consisting of

  • Halogen lamp
  • Adjustable parabolic mirrors
  • Screen for Schlieren optics
  • Image Recorder

Interchangeable test sections: Three test sections with different Mach Number:

  • subsonic

 

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