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Aerodynamic Characteristics of Airfoils at High Speeds (1925)
NASA Technical Reports Server (NTRS) · leaf 14
« … .GO .32 .36 .4tt .OO .0-^ .08 .12 J6 .20 .24 .28 .32 .36 00 .04 .08 .12 .16 .20 .24 .28 Drag coefficient, Cj, Drag coefficient Q> Drog coefficient Cj> FiQ. 32 riQ.30 Fig. 28 o M I o H Oh O 0^ .00 .04 .08 ,12 .16 .20 .24 .28 .32 .36 .00 .04 .08 .12 .16 .20 .24 .28 .32 .36 \00 .04 .08 .12 .16 .20 .24…NASA Technical Reports Server (NTRS)
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