International Journal For Multidisciplinary Research

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Behaviour of Whitcomb Integral Supercritical airfoil at various angles of attack in sonic condition using CFD

Author(s) SHAWN VARGHESE S, LS MADHUMITHA
Country India
Abstract Understanding the aerodynamic behaviour of an airfoil is crucial for evaluating its performance in generating lift and drag. In this study, the aerodynamic performance of the Whitcomb Integral Supercritical Airfoil is analysed across a range of angles of attack—specifically, 2°, 4°, 6°, 8°, and 10°—under sonic conditions. The primary objective is to investigate and characterize the lift and drag properties exhibited by the airfoil at these various angles of attack. This analysis will provide insights into how the airfoil performs in terms of efficiency and stability at sonic speeds.
Keywords Understanding the aerodynamic behaviour of an airfoil is crucial for evaluating its performance in generating lift and drag. In this study, the aerodynamic performance of the Whitcomb Integral Supercritical Airfoil is analysed across a range of angles of attack—specifically, 2°, 4°, 6°, 8°, and 10°—under sonic conditions. The primary objective is to investigate and characterize the lift and drag properties exhibited by the airfoil at these various angles of attack. This analysis will provide insights into how the airfoil performs in terms of efficiency and stability at sonic speeds.
Field Engineering
Published In Volume 6, Issue 5, September-October 2024
Published On 2024-10-12
Cite This Behaviour of Whitcomb Integral Supercritical airfoil at various angles of attack in sonic condition using CFD - SHAWN VARGHESE S, LS MADHUMITHA - IJFMR Volume 6, Issue 5, September-October 2024. DOI 10.36948/ijfmr.2024.v06i05.28422
DOI https://doi.org/10.36948/ijfmr.2024.v06i05.28422
Short DOI https://doi.org/g79447
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