COMPUTATIONAL METHOD FOR UNSTEADY MOTION OF TWO-DIMENSIONAL AIRFOIL

COMPUTATIONAL METHOD FOR UNSTEADY MOTION OF TWO-DIMENSIONAL AIRFOIL

A numerical method is developed for calculation of the wake geometry and aerodynamic forces on two-dimensional airfoil under going an arbitrary unsteady motion in an inviscid incompressible flow (panel method). The method is applied to sudden change in airfoil incidence angle and airfoil oscillatio...

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Bibliographic Details
Main Author: Anmar H. Ali
Format: Article
Language:English
Published: University of Baghdad 2024-02-01
Series:Journal of Engineering
Subjects:
Airfoil Oscillations, Panel Method, Unsteady Aerodynamics, Aerodynamic Coefficients, Hydrofoils, Lift, Pressure Distribution
Online Access:https://joe.uobaghdad.edu.iq/index.php/main/article/view/2445

Internet

https://joe.uobaghdad.edu.iq/index.php/main/article/view/2445

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