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The document contains solutions to midterm exam problems in aerodynamics, specifically addressing the superposition of uniform flow with sources and sinks, the NACA 4412 airfoil, and a rectangular airfoil with specified parameters. It provides mathematical formulations for stagnation points, center of pressure, lift coefficients, and induced drag coefficients. Each problem is solved step-by-step, detailing the necessary calculations and conditions for the results.

Author

Alex Pellicane

Language

EN