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1
WIND TUNNEL
TESTING
Wind Tunnels
Objective
• Accurately simulate the fluid flow about
atmospheric vehicles
• Measure -Forces, moments, pressure, shear
stress, heat transfer, flow field
2
Working of wind tunnel
3
WIND TUNNEL LAYOUTS
 Closed Return
 Open Return
 Double Return
 Annular Return
4
5
Closed Return(OpenTest Section)
6
15 Hp. Dual
Centrifugal Blower
Exhaust
Exhaust
Louvers
for Speed
Adjustment
Test Section
18 inch Diameter
25 to 1 Contraction
Screens High Contraction Wind Tunnel
Top View
Diffuser
Open Return(Closed Section)
7
Double Return
8
Annular Wind
Tunnel
TYPES OF WIND TUNNELS
 Subsonic
 Transonic
 Supersonic
 Hypersonic
 Specialty (Automobiles)
9
SUBSONIC TUNNELS
 Low speed wind tunnels are used for
operations at very low mach
number(M<0.5), with speeds in the test
section up to 480 km/hThey may be of
open-return type with air moved by a
propulsion system.
10
11
80X120
NASA AMES
12
80x120 WindTunnel
NASA Ames
13
12 Foot PressureTunnel
TRANSONIC WIND TUNNELS
 High subsonic wind tunnels (0.4 < M < 0.75)
or transonic wind tunnels (0.75 < M < 1.2)
are designed on the same principles as the
subsonic wind tunnels.
14
TRANSONIC WIND TUNNEL
 Testing at transonic speeds presents
additional problems, mainly due to the
reflection of the shock waves from the walls
of the test section
15
16
8x6 Functions & Capabilities
The 8x6 Foot Supersonic WindTunnel provides
customers with a Facility capable of testing large
scale aero propulsion hardware
Relative altitude 1000 - 35000 ft
Dynamic Pressure 3.6 - 4.8 x 106/f
Temperature 60 - 250oF
17
8X6AT NASA LEWIS
SUPERSONIC WIND TUNNELS
 A supersonic wind tunnel is a wind tunnel
that produces supersonic speeds (1.2<M<5)
The Mach number and flow are determined
by the nozzle geometry.
18
19
20
21
HYPERSONIC WIND TUNNELS
 A hypersonic wind tunnel is designed to
generate a hypersonic flow field in the
working section.
 The speed of these tunnels vary from Mach
5 to 15.
22
23
24
AUTOMOBILE WIND TUNNELS
External flow tunnels - Used to study the
external flow through the chassis
 Climatic tunnels - Used to evaluate the
performance of door systems, braking
systems etc. under various climatic
conditions.
25
26
TYPES OF WIND TUNNEL
TESTING
 ForceTest
 Force measurement requires a force to be
exerted (lift & drag forces so termed force
test)
 The balance can measure only two forces:
lift & drag
27
28
TYPES OF WIND TUNNEL
TESTING
 PressureTests
 Insert tiny tubes into the model surface or
airstream and connect them to a pressure
measuring device
29
 PressureTest:
 Lowered pressure over the wing surface
reduced the pressure in the manometer
tubes and draws the water level up to a high
level
 The lower the pressure, the higher the water
level goes
30
TYPES OF WIND TUNNEL
TESTING
 Flow Patterns
 Allow the streamlines of air flow to look at
the body’s aerodynamic properties
 Tufting allows for the flow pattern
visualization
31
32
Flow Patterns
INSTRUMENTS USED IN
WIND TUNNELS
 1.Force Balance
 2.Static Pressure Measurement
 3.Strain gauge
 4.Spring Gauge
 5.Laser DopplerVelocimetry
 6.Laser Sheet
33
FORCE BALANCE
34
STATIC PRESSURE
MEASUREMNT
35
STRAIN GAUGE
36
SPRING GAUGE
37
LASER DOPPLER
VELOCIMETRY
38
LASER SHEET
39
HOW ARE CARS TESTED IN
WIND TUNNELS??
 It is used to quantify and validate what is going
on aerodynamically to the vehicle by
measuring forces exerted on the body through
a 6 component balance.
40
HOW ARE CARS TESTED IN
WIND TUNNELS??
 Adding a rear wing to your car might gain you
down force, but a wind tunnel will tell you in
fact if it is, how much, and how it affected the
overall front to rear balance of your car.
41
HOW ARE CARS TESTED IN
WIND TUNNELS??
 Each test will output the drag, down force
(front & rear), and side force (front &
rear), yaw/pitch/roll moments, in order to see
the big picture of what is really happening for
any given configuration.
42
43
Few
Examples
44
COST OF A WIND TUNNEL
 A high quality portable vertical wind tunnel
will cost you anywhere from 1.6crores to
4.1crores.This type of tunnel can
accommodate skydivers as well as tourists.
45
WIND TUNNELS IN THE
WORLD
1.Altitude IcingWindTunnel(Ontario Canada)
2.Wright BrothersWindTunnel(MIT
Massachusetts USA)
46
47
WIND TUNNELS IN THE
WORLD
 3.WindTunnel at NASA Ames (World’s
Largest USA)
 4.Langley Low PressureTurbulenceWind
Tunnel(NASAVirginia USA)
48
49
REFERENCES
 www.wikipedia.com
 www.nasa.org
50
THANK YOU
51

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Wind tunnel testing aerospace

  • 2. Wind Tunnels Objective • Accurately simulate the fluid flow about atmospheric vehicles • Measure -Forces, moments, pressure, shear stress, heat transfer, flow field 2
  • 3. Working of wind tunnel 3
  • 4. WIND TUNNEL LAYOUTS  Closed Return  Open Return  Double Return  Annular Return 4
  • 6. 6 15 Hp. Dual Centrifugal Blower Exhaust Exhaust Louvers for Speed Adjustment Test Section 18 inch Diameter 25 to 1 Contraction Screens High Contraction Wind Tunnel Top View Diffuser Open Return(Closed Section)
  • 9. TYPES OF WIND TUNNELS  Subsonic  Transonic  Supersonic  Hypersonic  Specialty (Automobiles) 9
  • 10. SUBSONIC TUNNELS  Low speed wind tunnels are used for operations at very low mach number(M<0.5), with speeds in the test section up to 480 km/hThey may be of open-return type with air moved by a propulsion system. 10
  • 14. TRANSONIC WIND TUNNELS  High subsonic wind tunnels (0.4 < M < 0.75) or transonic wind tunnels (0.75 < M < 1.2) are designed on the same principles as the subsonic wind tunnels. 14
  • 15. TRANSONIC WIND TUNNEL  Testing at transonic speeds presents additional problems, mainly due to the reflection of the shock waves from the walls of the test section 15
  • 16. 16 8x6 Functions & Capabilities The 8x6 Foot Supersonic WindTunnel provides customers with a Facility capable of testing large scale aero propulsion hardware Relative altitude 1000 - 35000 ft Dynamic Pressure 3.6 - 4.8 x 106/f Temperature 60 - 250oF
  • 18. SUPERSONIC WIND TUNNELS  A supersonic wind tunnel is a wind tunnel that produces supersonic speeds (1.2<M<5) The Mach number and flow are determined by the nozzle geometry. 18
  • 19. 19
  • 20. 20
  • 21. 21
  • 22. HYPERSONIC WIND TUNNELS  A hypersonic wind tunnel is designed to generate a hypersonic flow field in the working section.  The speed of these tunnels vary from Mach 5 to 15. 22
  • 23. 23
  • 24. 24
  • 25. AUTOMOBILE WIND TUNNELS External flow tunnels - Used to study the external flow through the chassis  Climatic tunnels - Used to evaluate the performance of door systems, braking systems etc. under various climatic conditions. 25
  • 26. 26
  • 27. TYPES OF WIND TUNNEL TESTING  ForceTest  Force measurement requires a force to be exerted (lift & drag forces so termed force test)  The balance can measure only two forces: lift & drag 27
  • 28. 28
  • 29. TYPES OF WIND TUNNEL TESTING  PressureTests  Insert tiny tubes into the model surface or airstream and connect them to a pressure measuring device 29
  • 30.  PressureTest:  Lowered pressure over the wing surface reduced the pressure in the manometer tubes and draws the water level up to a high level  The lower the pressure, the higher the water level goes 30
  • 31. TYPES OF WIND TUNNEL TESTING  Flow Patterns  Allow the streamlines of air flow to look at the body’s aerodynamic properties  Tufting allows for the flow pattern visualization 31
  • 33. INSTRUMENTS USED IN WIND TUNNELS  1.Force Balance  2.Static Pressure Measurement  3.Strain gauge  4.Spring Gauge  5.Laser DopplerVelocimetry  6.Laser Sheet 33
  • 40. HOW ARE CARS TESTED IN WIND TUNNELS??  It is used to quantify and validate what is going on aerodynamically to the vehicle by measuring forces exerted on the body through a 6 component balance. 40
  • 41. HOW ARE CARS TESTED IN WIND TUNNELS??  Adding a rear wing to your car might gain you down force, but a wind tunnel will tell you in fact if it is, how much, and how it affected the overall front to rear balance of your car. 41
  • 42. HOW ARE CARS TESTED IN WIND TUNNELS??  Each test will output the drag, down force (front & rear), and side force (front & rear), yaw/pitch/roll moments, in order to see the big picture of what is really happening for any given configuration. 42
  • 44. 44
  • 45. COST OF A WIND TUNNEL  A high quality portable vertical wind tunnel will cost you anywhere from 1.6crores to 4.1crores.This type of tunnel can accommodate skydivers as well as tourists. 45
  • 46. WIND TUNNELS IN THE WORLD 1.Altitude IcingWindTunnel(Ontario Canada) 2.Wright BrothersWindTunnel(MIT Massachusetts USA) 46
  • 47. 47
  • 48. WIND TUNNELS IN THE WORLD  3.WindTunnel at NASA Ames (World’s Largest USA)  4.Langley Low PressureTurbulenceWind Tunnel(NASAVirginia USA) 48
  • 49. 49