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- W2138861443 abstract "insured that contact between the tube and wall occurred at the shoulder of the bevel. Very light contact could be detected by a change in electrical resistance with no bending of the tube. A micrometer attached to the tube-traversing mechanism could be set at zero at this point. Velocities in the boundary layer were determined from pitot pressure and tunnel supply pressure assuming constant total temperature. The data for all five surveys are tabulated in Ref. 4. The velocity profiles shown on Figs. 2 and 3 were obtained with the D = 0.020-in. and D = 0.095-in. tubes. The curve faired through the D = 0.020-in. data of Fig. 2 is reproduced on Fig. 3 for comparison with the D = 0.095-in. data. The D = 0.020-in. tube gives very nearly the correct results. Figure 3 demonstrates that the interference effects with a tube as large as D = 0.095 in. are quite small. The boundary-layer momentum thickness, 0, and displacement thickness, 6*, were determined from the data for each survey. In order to carry the integrations all the way to the wall, the velocity was assumed to vary with the |th root of distance in the region between the wall and the first survey point. Values of 0 and H = 6*/0 from Ref. 4, nondimensiona lized by values for zero tube diameter, are plotted on Fig. 4. Even with the largest tube (about 25% of the boundary-layer thickness), the error in 0 is only 2% and the error in H only 1%. In plotting the data from Ref. 4 vs D/S, it should be noted that S was taken as the thickness of a boundary layer with the entire velocity profile given by a ^th-root distribution. This fictitious boundary layer had the same 9 as the boundary layer surveyed." @default.
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- W2138861443 date "1973-10-01" @default.
- W2138861443 modified "2023-09-27" @default.
- W2138861443 title "Vibration of Orthotropic Circular Plates with a Concentric Isotropic Core" @default.
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- W2138861443 doi "https://doi.org/10.2514/3.50605" @default.
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