forms is to be expected because the separa- tion occurs back of the central plane for the circular 1.2 20 U6 .5 Reynolds Number o o o (based on width • V/Vc normal to stream) ■0./5 -o 2.1 x 10* -.4 ■ .20 x 2.8 - ■ .25 + 3.4 - .30 a 4.1 - i- O .4 .8 1.2 IS 20 2.4 Ratio of altitude to base, h/b Angle… … Figure 18.—Effect of shape on CDt. cylinder and at the central plane for the semitubular '1.6 cylinder. .7 .4 .5 .8 .2 Similarly, the drag coefficient of the triangular cylinder having a 90° apex angle wTith the apex to the Figure 16.—Variation In Cl with V/V, for the triangular cylinder having an…
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