Business Jet, Commercial and Regional Aircraft

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