Bayesian Forward Design Methodology for Laminar Transonic Airfoils with Cross Flow Attenuation at Large Sweep Angles

Drag reduction forms a key area of focus in aerodynamics with a significant emphasis on delaying the laminar-to-turbulent transition of boundary layers over the wings of aircraft. There is enough evidence to suggest that achieving such transition delays is particularly challenging for backward-swept...

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Bibliographic Details

Main Authors:	Samarth Kakkar, Thomas Streit, Arne Seitz, Rolf Radespiel
Format:	Artigo
Language:	Inglês
Published:	MDPI AG 2026-02-01
Series:	Aerospace
Subjects:	natural laminar flow crossflow attenuation CATNLF Bezier curves airfoil parameterization Bayesian optimization
Online Access:	https://www.mdpi.com/2226-4310/13/2/171
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