Experimental study of an optical fibre-based pressure sensor for boundary layer transition detection

Author:

Forte Maxime1,Seraudie Alain1,Arnal Daniel1,Molin Stephanie2,Vaudel Olivier2,Nouchi Pascale2

Affiliation:

1. ONERA

2. Thales Research & Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. Pressure measurements on aircraft wing using phase-shifted fibre Bragg grating sensors

2. 3Seraudie, A., and Forte, M. "JTI-SFWA WP1.3.7: Study of the detection of laminar-turbulent transition on a wing using optical fibre sensors (Phase2)," ONERA Technical Report, report n° 11/16609 DAAP/DMAE, Cleansky SFWA-ITD Confidential, 2011.

3. Experimental study for the detection of the laminar/turbulent aerodynamic transition on a wing aircraft, using fiber optic sensors

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1. Wind Tunnel Test;Encyclopedia of Ocean Engineering;2022

2. Wind Tunnel Test;Encyclopedia of Ocean Engineering;2020

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