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Pressure Drop Across Finned Cylinders Enclosed in a Jacket (1937)

NASA Technical Reports Server (NTRS) · leaf 28

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Fig. 11 H.A.C.A. Technical Note No. 631 V2 pav g ,1b./sec./sq.ft. 3 4 5 6 7 8 10 15 30 25 … 4 5 6 7 8 10 15 20 35 v3 Pav S .lb./sec./sq. ft. Figure 11.- Effect of radii of skirt approach on pressure drop across the -2- - l-i- and — - 1— cylinders. Entrance and exit ratios 1.6 8 3 33 3

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