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Source Panel Method in Aerodynamics by Mano Har is a document available to read on EtoBox.
What is Source Panel Method in Aerodynamics about?
The document summarizes an aerodynamics project using a source panel method to model airflow over an airfoil. The student used MATLAB code to calculate pressure coefficients (Cp) and understand how they vary with angle of attack. The Cp curves matched theoretical values. Cl and Cd values approached zero as expected for inviscid, non-rotational flow at zero angle of attack. Cp curves were symmetric for equal but opposite angles of attack.
- Author
- Mano Har
- Language
- EN