ONERA Wind Tunnel Division test facilities offer large capabilities for testing civil aircraft, with complete model, half (motorized) model or components (air intake, landing gear ...) in the different flight phases (take of, 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
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Half model test in S1MA
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F7X model in S2MA
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Technical documentation