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Wind-tunnel tests of a Clark Y wing with 'Maxwell' leading-edge slots (1937)
NASA Technical Reports Server (NTRS) · leaf 9
Fig. 3 t.A.O.A. Teohnioal Hote Ho. 598 … Slat otdinates in peroent of alat ohord Station 0 5. 10 16 20 36 30 35 40 45 ■ 50 55 60 65 70 75 80 86 ^ Ordinates from reference line. 1.37 4.01 90 T.E. radius 0.23 peroent slat ohord .67 3.34 95 Figure 3.-The Olarlc T wing with 0.30 o. Maxwell slat, with and without a split flap .33 100NASA Technical Reports Server (NTRS)
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