The Drag of Two Streamline Bodies as Affected by Protuberances and Appendages (1934)
NASA Technical Reports Server (NTRS) · leaf 6
g this model with the rear support net bare-hull drags. wires in two positions. The static pressure gradients were measured at all tank pressures (reference 7) for RESULTS AND DISCUSSION the determination of the horizontal buoyancy correc- tion, which was computed for each pressure by a pro- The… … Reynolds Number, based on the over-all length of I he model Figure 4.—Drag coefficients of model A Tested in the N. A. C. A. variable-density wind tunnel. Volume=0.472 cu. ft. (Vol.) 2/3=0.6C6 sq. ft. Length = 37.39 in. Bare hull with original and altered sterns. Drag coefficient and Reynolds…
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