ONERA Wind Tunnel Division test facilities offer large capabilities for testing civil aircraft, with complete model and half model (motorized or non-motorized), or components (air intake, landing gear ...) in the different flight phases (take off, cruise, landing, limit of the flight envelope conditions ...).
- Flight performances
- Stability and Control
- Dynamic stability
- Flutter
- Ground floor effect
- Wake survey
- Laminarity tests
- Rear end measurements
- Noise measurements
- Installed Propulsion Performance
- Isolated Propulsion Performance
- Isolated component test: air intake test performances, APU, landing system
- Propeller driven aircraft
Air inlet test in F1
|
Half model test in S1MA
|
F7X model in S2MA
|
Technical documentation