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Aerodynamic Characteristics of Airfoils at High Speeds (1925)
NASA Technical Reports Server (NTRS) · leaf 14
« I.I 1.0 €0 0.9 0.8 ^0.7 C ^0,6 (fi lo.s u ^0.4 0.3 9 0.2 0.1 S3 0.0^ .04 .08 .12 .16 .20 .24 .28 .32 .36 .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 … .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 .28 .32 .36 .40 Drog coefficient, G Drag coefficienfj Co Co Drag coefficient. Fio.29 FiQ. 31 Fig. 83 Polar diagrams, Cl vs. Cd. Various values of VicNASA Technical Reports Server (NTRS)
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