Contact us
en
Français
About ONERA
News
Events
Centers
International
Press
Our activity
Research - Aeronautics Space Defense
Scientific Strategy
Research at ONERA
Strategic Scientific Plan
Looking to the future
A high performance computer
Scientific High Council
Scientific Domains
Materials and Structures
Fluid Mechanics and Energetics
Physics
The Advanced Numerical Simulation Domain
Information Processing and Systems
Doctoral theses and post-doctoral contracts
Scientific Publications
Lessons, presentatons, conferences
Focus ONERA
Programmes
General Technical Director's viewpoint
Aeronautics
Space
Defense
Research integrity and research ethics at ONERA
Scientific Departments
DAAA - Aerodynamics Aeroelasticity Acoustics
Missions
Scientific topics
Research units
Technical resources
Contact
DEMR - Electromagnetism and Radar
Missions
Scientific topics
Research units
Technical resources
Contact
DMAS - Materials And Structures
Missions
Scientific topics
Research units
Technical resources
Contact
DMPE - Multi-physics department for energy
Missions
Scientific topics
Research units
Contact
DOTA - Optics and Associated Techniques
Missions
Scientific topics
Research units
Contact
PHY - Physics Instrumentation Environment Space
Missions
Scientific Topics
Research units
Technical resources
Contact
DTIS - Information Processing and Systems
Missions
Scientific topics
Research units
Technical resources
Contact
Wind Tunnels
Testing services
Overview on our capabilities
Non conventional tests
Business Jet, Commercial and Regional Aircraft
Military Aircraft
Missiles and launchers
Propeller powered aircraft
Helicopter and convertible
Space application
Testing Capabilities
Wind tunnel facilities
Balance Calibration Laboratory
F1
F2
CEPRA19
S1MA
S2MA
S3MA
S4A
S4B : TPS calibration
BD2 : Nozzle thrust measurement
Testing techniques
Overview on various measurement methods and testing techniques
Propulsion Simulation
Model Load Measurement
Model deformation measurements
Model Pressure Measurement
Flow field survey and visualization
Acoustic Measurement
Model Attitude Measurement
Heat flux measurement
Transition tripping and visualization
Model support
Model Preparation
Data Acquisition and Processing
Video and Photographic Monitoring
Store Release Simulation
Design and manufacture capabilities
Overview
Engineering and Capital Project Support
Wind Tunnel Model
Balance design capability
Quality management
Contact Wind Tunnels
Valorization
Our offer
Our achievements
Resources
Home
The French aerospace lab
Share this page
The French aerospace lab