CORDIS Project
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This project focuses on wind tunnel testing of a half model wing designed for natural laminar flow. It investigates how surface imperfections affect airflow, aiming to enhance aerodynamic performance in aviation.
The main objective of the present proposal is the performance of wind tunnel testing of a half model at transonic speed and near flight Reynolds number.
The model wing featuring a natural laminar flow (NLF) design will be subject to artificially generated surface steps and imperfections allowing investigating the resulting effect on the flow behaviour on the wing.
The proposed activities comprise the design and provision of a controlled high pressure air supply inside the model, the model prepar…
EUROPEAN TRANSONIC WINDTUNNEL GMBH
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