HM 18S WIND TUNNEL

 

Description

 

WIND TUNNEL has been developed to perform various experiments of aerodynamics and fluid flow.  An open circuit Wind Tunnel consists of a region of uniform air flow into which different models can be fitted.

The wind tunnel has bell mouth shaped entry to guide the air smoothly into test section. Air entry of wind tunnel has one honey comb grid and nylon mesh screens which stabilizes the air flow.

Test section with transparent acrylic sheet, is provided for visual observation. Diverging section of the wind tunnel acts like a diffuser reducing the dynamic pressure of air at the exit.

An axial fan coupled with variable speed AC motor is used to attain desired wind velocity. A Variable Frequency Drive motor control is used for testing various aerodynamic models at various air velocities.

An optional computerized version of wind tunnel is also available. Various graphs can be plotted by interfacing the equipment via National Instruments Labview based software. Data logging in MS Excel

 

EXPERIMENTS

 

  • To plot speed curve for wind tunnel with velocity of wind
  • To study pressure distribution around aerofoil, Cylinder etc.
  • To measure lift and drag force on aerofoil model etc.
  • To study the development of boundary layer along a body in Tunnel

 

Features

 

  • Compact & stand alone set up
  • Superb Painted structure
  • Easy to operate & minimum maintenance required.

 

UTILITIES REQUIRED

 

  • Electric Supply:C. 3 phases 440 volt, 50 Hz with neutral and Earth
  • Floor Area 10 x 3.5 m

 

TECHNICAL DETAILS

 

Product & Code sub sonic Wind tunnel HM 18S
Type of Wind Tunnel Open Type Wind Tunnel Low speed, open circuit, suction type

Approx velocity 25 to 30 m/sec

Wind Tunnel

Construction details MOC & Size

Wood ( Hunsur – Mysore /Ghana teak)

Plywood: 710 grade 3 mm thick for curved section,  7-8 mm for straight sections

18mm plywood to be used for making test section

of contraction, transition, diffuser and,

Fan Duct Made of MS

Effuser: Made of wood (Hunsur-mysore/Ghana teak) with MS support

Diffuser: Square to round section of 600 mm Diameter made of Contraction ratio CR of body with MS support

Total Length 7.50 to 8.00 m

Contraction ratio: 9:1

Honey comb: 8:1

Test Section 300x 300 x 600mm (length) with acrylic windows on either side of the test section.

Top opening and provision to place the traverse / pitot static tube along the length of the test section.

Provision for lighting the test section.

A turn table at the bottom of the test section for mounting models.

Fan Unit Axial flow with rigid MS support / frame

Motor of Capacity 2.2 KW, 1450 RPM with Variable Speed AC Drive

Ac Motor Controller/ Drive

– Variable frequency drive.

– High performance V/F control with both closed & open loop control .

– Digital display RPM. Voltage & current , power O/P in KVA and KW

– touch keypad for varying motor RPM, Start & Stop,

Wind Tunnel Accessories
Air Velocity Measurement Pitot Static Tube: Prandyl type

Static Tube: Prandyl type

Total Pressure Tube: Prandyl type

By pitot tube 24 to 28 m/s length 350 mm, Tube Diameter ¼”

With Digital pressure indicator & U tube manometer

2 Component Balance Lift force and drag force

Lift- 10 Kg.

Drag- 3 Kg

Strain gauge with amplifier with digital indicator

2D Transverse Motorized X- Axis along the flow & Y-Axis perpendicular to the tunnel

Range: 350mm

Compact & uses linear movement block (LM Block) for rigidity of the movement and ball-screw nut for manual as well as motorized controlled movement of the LM block

Diameter of the screw 15mm, Pitch of the screw 5mm

Linear scale fixed to the support gives 1mm readings.

Circular disc fixed to the shaft of the screw gives has 100 divisions on the circumference. This gives a movement 0.05 mm / division.

A disc with a handle is provided for continuously rotating the screw for movement of the traverse when the movement is mechanical.

Symmetric & Cambered Aerofoil NACA-662015, 150mm chord length, 15% thick.

Symmetrical aerofoil model for lift-drag study

Symmetrical aerofoil model for pressure distribution study With 15 pressure ports

Multiple Tube Manometer 15-20 x 400mm ht PVC Tubes 0-45° inclination with vertical axis with separate Stand for pressure distribution study
Smoke generator Smoke generator using liquid parofin and smoke rake to suit the above tunnel
Control Panel Consisting of

Digital lift drag indicator

Variable Speed AC Drive with digital speed indicator

Digital pressure indicator & U tube manometer of Pitot tube arrangement

Extra Accessories Optional Available
Cylinder 50mm dia with 20 pressure ports
Wake Rake 20 ports
Boundary Layer Rake 15 ports with surface plate
Projection Manometer An instrument for measuring differential pressure, in the range of 0-300mm Water/Alcohol head. The above manometer is used for measurement of wind speeds in wind tunnel and ducts up to a speed range of 0 to nearly 30meter/sec.

The projection manometer can also be used for measurement of differential air pressure in the range of 0 psi to about 0.45 psi. The projection manometer is an accurate instrument, easy to use and rugged. The accuracy of this instrument is 0.1mm height of the liquid used.

 

 

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