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Wind-tunnel investigation of the aerodynamic balancing of upper-surface ailerons and split flaps (1937)
NASA Technical Reports Server (NTRS) · leaf 12
THE AERODYNAMIC BALANCING OF UPPER-SURFACE AILERONS AND SPLIT FLAPS 171 … d. , degrees .005 oos .004 .004 003 003 002 002 .001 OOI ,-.00/ ,-■00/ -IOO -80 -60 -40 -20 -100 -80 -60 -40 -20 6a , degrees 6a .degrees Figure 22.—Honing-, yawing-, and hinge-moment characteristics of balanced upper- Figure 23.—Rolling-, yawing-, and hinge-moment characteristics of balanced…NASA Technical Reports Server (NTRS)
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