The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing (1934)
NASA Technical Reports Server (NTRS) · leaf 10
3 > 10 8't o !> ^atCL I max BatCLmax S Center removed 0.15 c tapered c flap - Tips removed o o. 15 0 constant c flap S5 n -0.25c tapered c flap A 0.25 c constant c flap- O … 10 Flap deflection, degrees, 6> + . Figure 9.- Effect of partial-span spht m flaps on CLmox and on CD and In Figure 6 - Effect of flap shape and deflection on The 0.15 c tapered-chord L/D at CLinax 05 r. and on L/D at CLmax for 5:1 flaps on 5:1 tapered wing,5F* 6G°- CD tapered wing
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