Aerodynamic characteristics of wings with cambered external airfoil flaps, including lateral control, with a full-span flap (1936)
NASA Technical Reports Server (NTRS) · leaf 15
REPOKT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS 12 .14 '- 5° 20" er -25" -5° o- .12 '-25° 20 ° x (Measured) ~ -25" 20" — + --- (Estimated? … ci, degrees Figure 30.—C and C„', 0.20 c Clark Y flaps on N. A. C. A. 23012 wing. Semispan ailerons deflected separately and together. .10 -.01 .08 .06 -.03 0 8 16 d, degrees Figure 32.—CV, N. A. C. A. 23012 wing with external-airfoil flaps and ailerons .04 (0.20 c flap). Aileron span=6/4. ,02 C,'…
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