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Fundamental and Experimental Aerodynamics

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DAFE Site Map

ONERA DAFE: 2D and 3D Particle Image Velocimetry (PIV)

PIV at ONERA DAFE: equipment

Two-component plane PIV at ONERA DAFE

Three-component or Stereo plane PIV at ONERA DAFE

Tomographic PIV

ONERA DAFE DTIM: FOLKI-SPIV software: fast and accurate stereo PIV vector processing based on GPU

Aerospace Lab Particle Image Velocimetry (ALPIV)

S3 Wind-Tunnel with return Circuit and Continuous Operation

S3 Transonic Wind-Tunnel - Control of Mixture at Nozzle Exit

S3 Transonic Wind-Tunnel - ATAC Launch Vehicle Afterbody

S3 Transonic Wind-Tunnel - OAT15A Wing Profile in Critical Regime

S3 transonic wind tunnel with return circuit and continuous operation

Control of mixture at nozzle exit

Study of ATAC launch vehicle afterbody

Study of an OAT15A wing profile in critical regime

Turbine Test Bench VEGA2

R3Ch and R5Ch Hypersonic Wind Tunnels

DAFE Computation Codes

Base and Afterbody Flow Modelling

PSP, Pressure Sensitive Paint

PSP, Pressure Sensitive Paint, Application to Hypersonics

PSP, Pressure Sensitive Paint - Application to Low Speeds

Viscous Interactions and Separation in Hypersonic Flow

Mars Sample Return Orbiter in the R5Ch Hypersonic Wind Tunnel

Effect of a plasma in supersonic flow

Image Resection

Image Resection

Last Update: 7 February 2012 - © ONERA 2009 - Terms of use