Propeller powered aircraft

ONERA Wind Tunnel Division test facilities offer large capabilities for testing civil aircraft, with complete and half models (motorized or non-motorized) or with components (air intake, landing gear ...) in the different flight phases (take off, cruise, landing, limit of the flight envelope conditions ...).

  • Isolated propeller performances
  • Integrated propeller performances
  • Acoustic measurements
  • RSB using (with telemetry if necessary) for load measurements - 6 components

Open rotor test capabilities : Specific test rigs for isolated propeller and installed effect measurements development ongoing (isolated configuration operational since 2013).

A400M model on straight sting in S1MA

A400M model on mono-strut in F1


Technical documentation