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Wind-tunnel research comparing lateral control devices, particularly at high angles of attack IX : tapered wings with ordinary ailerons (1933)
NASA Technical Reports Server (NTRS) · leaf 26
H.A.C.A. Technical ITote Ho.449 Tig. 3 /T'tX T^T \ / £5' 85° \ / < /- <i—/- Equal up-and-down Differential No. I … Differential No.2 (50e ZS/S/S/SS/ssss,— v ^ Up-only Figure 3.-Aileron linkage systems-assumed maximum, deflections.NASA Technical Reports Server (NTRS)
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