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 25
2 > Note: Hinge axis of spoilers A and C … ? 30.00"- 30.00" ■40%g- —I 40%c 1 50%^ eo%? 10%c ^Spoiler D ^Spoiler A Spoi ler C -11 Spoiler C Figure 1.-Clark Y wing model with auxiliary airfoil, two sizes of ailerons and three types of spoilers. on
NASA Technical Reports Server (NTRS)
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