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Wind tunnel research comparing lateral control devices, particularly at high angles of attack VIII : straight and skewed ailerons on wings with rounded tips (1933)

NASA Technical Reports Server (NTRS) · leaf 16

An illustration from Wind tunnel research comparing lateral control devices, particularly at high angles of attack VIII : straight and skewed ailerons on wings with rounded tips, 1933, leaf 16
M.A.C.A. Teohnical Note Ko.445 Fig. 3 —/—f 4- \ / V/ y • v A, Equal up-and-down … -Xf57 / / \ I I Cj Extreme different/a/ (No.2) t L \ f V i f \ J D, Up-only Figure 3. Aileron linkage systems - assumed maximum deflections.

NASA Technical Reports Server (NTRS)

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