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


Technical documentation