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Theoretical and Applied Optics

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Aero-optical effects


Striogram of flow in the vicinity of a cavity


Numerical simulation of the flow

Objective

Numerical and experimental characterization of the effects of aerodynamic flows at transonic speeds around aircraft for the development of statistical aero-optical models.

Participants ONERA

DOTA, DAAP, DAFE, DSNA, DMAE et DMPH.

 


Characterization setup
(S8 wind tunnel)

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Last Update: 30 November 2006 - © ONERA 2009 - Terms of use