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What is L11 Fall25 about?

The document covers Prandtl’s Lifting Line Theory, focusing on lift distribution, drag, and the significance of elliptical lift distribution for minimizing induced drag. It includes calculations for lift and drag coefficients for a rectangular wing and discusses the impact of wing design, such as swept wings, on drag during different flight conditions. The content is part of an Aerodynamics course led by Dr. Baris Gungordu at METU.

Author

mustafa16ciftci

Language

EN