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Fundamental and Experimental Aerodynamics

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S3 Transonic Wind-Tunnel
Study of ATAC Launch Vehicle Afterbody


Axisymmetrical model on an upstream
with change of base configuration,
jet simulation (0.650kg/s),
with adaptation of test section walls

Measurement of steady and unsteady pressures

Schlieren and shadowgraph visualizations

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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