CORDIS Project
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This project focuses on delaying the transition from laminar to turbulent flow on aircraft wings to reduce drag and fuel consumption. By utilizing advanced measurement techniques and a novel active flow control system, it aims to enhance aerodynamic efficiency in aviation.
Delay of laminar-turbulent flow transition on aircraft wings can potentially reduce aerodynamic drag by up to 15%, reducing emissions and fuel consumption considerably.
The main cause of laminar-turbulent transition on commonly used swept wings is the development of crossflow (CF) instabilities.
Despite their importance, our fundamental understanding of CF instabilities is limited due to inability of current measurement techniques to capture their complex and multi-scale spatio-temporal features…
TECHNISCHE UNIVERSITEIT DELFT
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