The Effect on Lift, Drag, and Spinning Characteristics of Sharp Leading Edges on Airplane Wings (1933)
NASA Technical Reports Server (NTRS) · leaf 21
T … \ with Reference 3 \ vClarkY, R.N. 3,250,000, V.D.T. test 525] — " Y-B, R.N. 3,120,000, V.D.T. test 838-2 I 1 I 1 I I 1 I I I I .4 .6 .8 1.0 1.2 1.4 1.6 Lift coefficient, CL Figure 5 -Profile drag
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