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Applying the results of experiments on small models in the wind tunnel to the calculation of full-sized aircraft (1922)

NASA Technical Reports Server (NTRS) · leaf 17

An illustration from Applying the results of experiments on small models in the wind tunnel to the calculation of full-sized aircraft, 1922, leaf 17
+ attachments on upper camber. O " ■ " lower » O spatula « « » … ■ Angle of attack. Aerofoil E 308 B on page 16. Table of characteristics on page 35, Fig. 2 (Continued on page 13).

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