Laminar-Turbulent Transition in Swept-Wing Flows with a Supercritical Forward-Facing Step
Book Chapter
(2024)
Author(s)
J. Casacuberta Puig (TU Delft - Aerodynamics)
S. Hickel (TU Delft - Aerodynamics)
M. Kotsonis (TU Delft - Aerodynamics)
Research Group
Aerodynamics
Copyright
© 2024 J. Casacuberta Puig, S. Hickel, M. Kotsonis
DOI related publication
https://doi.org/10.1007/978-3-031-47028-8_23
To reference this document use:
https://resolver.tudelft.nl/uuid:984278af-7a31-498b-9768-0af914f606f1
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Publication Year
2024
Language
English
Copyright
© 2024 J. Casacuberta Puig, S. Hickel, M. Kotsonis
Research Group
Aerodynamics
Bibliographical Note
Green Open Access added to TU Delft Institutional Repository ‘You share, we take care!’ – Taverne project https://www.openaccess.nl/en/you-share-we-take-care
Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public.
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Pages (from-to)
151-156
Reuse Rights
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Abstract
Achieving and maintaining laminar flow on large swept lifting surfaces of subsonic aircraft poses a considerable challenge.
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