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
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A400M model on mono-strut in F1
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Technical documentation