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Author

Florin Mihaila

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Open access Jul 2026

Hover Performance and Uncertainty Quantification of a Light-Twin Helicopter Rotor

This study presents an extended Blade Element Momentum Theory (BEMT) framework for predicting the hover performance of an EC135-class light-twin helicopter rotor while quantifying the impact of sectional aerodynamic uncertainty on global rotor metrics. Because the proprietary EC135 airfoils are not publicly available,...

Florin Mihaila, Ion Fuiorea, G. Cican · 0 citations

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