= F3 Lecture Notes: Thin-Airfoil Analysis Problem, continued by MIT OpenCourseWare
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https://ocw.mit.edu/courses/16-01-unified-engineering-i-ii-iii-iv-fall-2005-spring-2006/d721171c42af48a056aaccec784a6d10_f03_0304.pdf
Originating MIT Unified Engineering teaching notes, hosted by MIT OpenCourseWare. No personal byline is established from the four-page PDF. Page 2 defines the camber-slope Fourier coefficients; p. 3 derives section lift and the zero-lift incidence; p. 4 explains angle-independent quarter-chord moment within thin-airfoil theory. The chord-to-angle substitution integrates over the angular interval from zero to pi; numerical examples in the concept articles are original calculations, not experimental results.
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