Re-examinations of the two-dimensionality of the flow and skin friction coefficient were made in a zero-pressure gradient, smooth wall, turbulent boundary layer. In order to well achieve the two-dimensionality, the balance in momentum integral equation was checked in detail. And, the wall shear stress was determined by direct measurement using a floating element device. The momentum thickness Reynolds number ranges from 840 to 6220. The present results of skin friction coefficient obtained by the direct measurement proposed an empirical formula, and the quantitative differences were evaluated between the formula and the available experimental results. On the logarithmic velocity profile, the values of Kármán constant, additive constant, and wake parameter are affected by the methods to estimate skin friction coefficient and a degree of reliability of the two-dimensional flow. The profiles of present turbulent quantities were measured carefully in the turbulent boundary layer to construct database of the two-dimensional turbulent boundary layer without pressure gradient.
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