Aerodynamic characteristics of wings with cambered external airfoil flaps, including lateral control, with a full-span flap (1936)
NASA Technical Reports Server (NTRS) · leaf 19
REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS 16 … Figuhe 46—C against A CD, N. A. C. A. 23012 wing with 0.20 c Clark Y external- airfoil flaps deflected as ailerons. Aileron span=6/4. Figure 44—C' against ACD, N. A. C. A. 23012 wing with 0.20 c Clark Y external- .14 airfoil flaps deflected as ailerons. Aileron span=6/2. .12 .12 0°,30° 0°5°,I0° 15°…
NASA Technical Reports Server (NTRS)
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