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Aerodynamic computation of gliders (1922)
Schrenk, · leaf 10
Angle of attack Fig. 1. Fie. 2-Airf oils 376 and 441. Aspect ratios 5 and 10. Fig. 4- Airfoil 441. Fig. 3-Air foil 376. Aspect ratio 5. A-apect ratio 5. p**)-' Figs. 1-2-3-4.Airplanes - design · Commercial airplanes
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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