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Wind-tunnels

Table of wind-tunnels and other aerodynamic facilities

Continuous Wind Tunnels

Facility
Location
Type
Power
Test section
Area or LxH
Speed
Mach number
Reynolds
number
(in Millions)
based on 0.1 racine de S
F1
Fauga
Continuous
pressurized
subsonic
9.5 MW  
4 model-carts
4.5x3.5 m2
inferieur ou egal 123 m/s
M inferieur ou egal 0.36
8
F2
Fauga
Continuous
atmospheric
subsonic
0.75 MW
1.4x1.8 m2 inferieur ou egal 100 m/s 1.1
CEPRA19
Saclay
 
a Continuous
atmospheric
aeroacoustic
7 MW
Open jet
Ø 2 m
inferieur ou egal 130 m/s 1.3
Open jet
Ø 3 m
inferieur ou egal 60 m/s 0.8
S1MA
Modane
Continuous
atmospheric
sub/transonic
88 MW
Cart #1:
40/42.6 m2

slotted walls
M < 1 7.3 / 7.5
Cart #2:
45 m2
solid walls
M < 1 7.7
Cart #3: 45.4/47 m2
solid walls
M < 1 7.7 / 7.9
Cart #4:
38.5 m2
anechoic walls
M inferieur ou egal 0.85 6.7
S2MA Modane Continuous
pressurized
sub/trans/
supersonic
55 MW
Transonic
1.75
x 1.77 m2
0.2 inferieur ou egal M inferieur ou egal 1.3 5.4
Supersonic
1.75 
x 1.93 m2
1.5 inferieur ou egal M inferieur ou egal 3.1 4.0

Blow-down Wind Tunnels

Facility
Location
Type
Power
Test section
Area or LxH
Speed
Mach number
Reynolds
number
(in Millions)
based on 0.1 racine de S
S3MA Modane Blow-down
pressurized
sub/trans/
supersonic
Transonic
0.56 x 0.78  m2
0.1 inferieur ou egal M inferieur ou egal 1.3 3.5
Supersonic
0.76 x 0.80 m2
1.65 inferieur ou egal M inferieur ou egal 5.5 3.2
S4MA Modane Blow-down
hypersonic
Ø 0.68 m M = 6.4 1.7
Ø 1 m M = 10 0.9
Ø 1 m M = 12 0.35
F4
Fauga
Arc heated
high-enthalpy
hypersonic
2.5 - 17 MJ/kg
Nozzle 1:
Ø 670 mm
8 < M < 17 2
Nozzle 2:
Ø 670 mm
7 < M < 13 3
Nozzle 3:
Ø 430 mm
6 < M < 11 5
Nozzle 4:
Ø 930 mm
9 < M < 21 1

other aerodynamic facilities

Facility
Location
Type Features Speed
Mach number
S4B
Modane
Model engine
calibration facility
(vacuum tank)
Test rigs for 4” to 9"
Turbine Power Simulators
and nozzles
Simulated Mach number
< 1 (TPS)
< 5 (nozzles)
BD2
Modane
Test bench for
nozzles / afterbodies
with heated core
and secondary floors
Mass-flow:
30 kg/s
Pressure:
25 bar
Temperature: 1150 K  
N/A
R4
Modane
Cascade wind-tunnel 2D width:
120 mm
Reynolds number:
3.3 106
(chord 100 mm)
M = 0.3 à 1.6
TURMA
Modane
Test rig with two turbine stages with different speeds of rotation. possibly contrarotating Mass-flow:
11 kg/s
Pressure:
4 bar
Temperature:
450K
Power:
HP 2MW ; BP 0.75MW
N/A

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Last Update: 17 March 2006 - © ONERA 2009 - Terms of use