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Wind tunnel research comparing lateral control devices, particularly at high angles of attack X : various control devices on a wing with a fixed auxiliary airfoil (1933)

NASA Technical Reports Server (NTRS) · leaf 27

An illustration from Wind tunnel research comparing lateral control devices, particularly at high angles of attack X : various control devices on a wing with a fixed auxiliary airfoil, 1933, leaf 27 — t. Figure 3.- Lift, drag, and center of pressure characteristics of different wing models with fixed auxiliary airfoils. «

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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