Measurements of Flow in the Boundary Layer of a 1/40-Scale Model of the U. S. Airship "Akron." (1933)
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den, H. L., and Kuethe, A. M.: Effect of Turbulence in u/ub= (y/5y/n where n is approximately 7 over the Wind-Tunnel Measurements. T. R. No. 342, N. A. C. A., central portion of the hull but decreases to 6.4 and 6.2 1930. near the forward and after extremities, respectively. 5. Millikan, Clark B.:… … 0.01 I'009 .006 .005 .004 .003 .ooa .001 8 /07 4 I06 a 3 4 5 G 8 to* VlvoLW* Reynolds Reynolds Number - -7— L h.t'KK 10.—Comparison of computed frictional drag (Millikan's equations) and experimental results -airship model Akron 6. Freeman, Hugh B.: Force Measurements on a 1/40-Scale Millikan's…
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