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Calculated effect of various types of flap on take-off over obstacles (1936)
NASA Technical Reports Server (NTRS) · leaf 21
r.A.C.A. Sechnical Note No. 568 Fig. 6 1, External-airfoil flap neutral 2, Plain flap 3, Balanced split flap 2000 H 1 1 f i 1 1— … 400 7 9 11 13 15 w/hp. Figure 6.-Variation of total take-off distance at Best flap angle with power loading. (Wing loading, W/s = 16-3)NASA Technical Reports Server (NTRS)
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