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When a full-scale airfoil cannot be tested in existing icing wind tunnel, the airfoil should be scaled. A hybrid airfoil is the scaled airfoil maintaining the leading edge of the full-scale airfoil. We show a method that can match distributions of important parameters in icing phenomenon. Then, it is confirmed that the method can minimize the discrepancy between full-scale and hybrid airfoils.

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This page is a summary of: Design of Hybrid Airfoils for Icing Tunnel Tests Based on Reduced-Order Modeling Methods, Journal of Aircraft, July 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c036435.
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