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FRANÇAIS


Fundamental and Experimental Aerodynamics

S3 Transonic Wind-Tunnel
Control of Mixture at Nozzle Exit


Setup of a ventilated nozzle model on the lower
wall reconstructing the phenomena encountered
on the M88 engine

Measurement of surface pressures

Observation and measurement in transverse and longitudinal planes


Exploration by motorized trident probe
(total pressure, static pressure and temperature)

 
Visualization by laser tomoscopy


Schlieren visualization


Shadowgraph visualization  


Measurement by particle image velocimetry

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Overview

Control of Mixture at Nozzle Exit

ATAC Launch Vehicle Afterbody

OAT15A Wing Profile in Critical Regime


Last Update: 11 June 2007 - © ONERA 2009 - Terms of use