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December 20, 2023Osmaniye Korkut Ata Üniversitesi Fen Bilimleri Enstitüsü Dergisi

Numerical Investigation of Flow Structure around NACA 0018 with slot

Ömer Fethi Aşan Emre Güler Muhammed Murat Aksoy Engin Pınar Tahir Durhasan

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Key Points

The slotted design enhances lift while delaying the stall angle of the airfoil.
CFD results were obtained at a constant Reynolds number of 3x105 for accuracy in comparisons.
Three different slot locations were examined, revealing significant aerodynamics improvements.
Higher angles of attack were assessed to evaluate the effectiveness of the airflow modifications.

Implication

CFD analysis demonstrates improved lift and delayed stall angle for NACA 0018 airfoil with slot, suggesting effective passive flow control.

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Cite This Study

Aşan et al. (2023) studied this question.

synapsesocial.com/papers/68c1e17854b1d3bfb60fef8c https://doi.org/10.47495/okufbed.1206762

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