@inproceedings{e9e51595844645299a1c639017221d04,
title = "Transition Due to Aerofoil-Wake Boundary Layer Interaction",
abstract = "The laminar-turbulent transition due to the interaction of an upstream aerofoil wake on a downstream flat plate boundary layer is studied experimentally. Measurements conducted on the flat plate boundary layer for four different aerofoil heights (hw ) above the flat plate demonstrate the evolution of both a non-modal disturbance profile and a longitudinal streaky structure in the pre-transition region. Sensitivity to aerofoil height suggests that this experimental arrangement would enable more systematic investigations of the receptivity mechanisms in multi-element configurations than possible using grid turbulence-induced transition.",
author = "Dhamotharan Veerasamy and Chris Atkin",
note = "Acknowledgements: The Authors would like to thank Prof. Michael Gaster for his advice and support. Gratitude is also extended to InnovateUK and ESPRC respectively for funding this project under the Enhanced Fidelity Transonic Wing project (InnovateUK grant ref. 113024, coordinated by Airbus) and the National Wind Tunnel Facility project (EPSRC grant ref. EP/L024888/1, led by Imperial College).",
year = "2021",
month = jul,
day = "31",
doi = "10.1007/978-3-030-67902-6_45",
language = "English",
isbn = "978-3-030-67901-9",
series = "IUTAM Bookseries",
publisher = "Springer",
pages = "521--527",
editor = "S. Sherwin and P. Schmid and X. Wu",
booktitle = "IUTAM Bookseries",
address = "Germany",
}