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Principles of Methods and Techniques in the Measurement
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according Aeronaut anemometer apply assumed assumption average axial boundary layer boundary-layer flow calculated coefficient of eddy consider const constant correlation function Corrsin curve cylinder decay determined diameter dissipation distance eddy diffusion eddy viscosity effect electric resistance energy spectrum equation of motion error curve Eulerian experimental expression flow field flow pattern fluid particles free jet free turbulent Gaussian gradient grid heat Hence homogeneous hot wire hot-wire incompressible fluid increases integral scale isotropic turbulence kinetic energy Lagrangian mean motion mean velocity measured momentum obtained pipe flow plane Prandtl pressure Proc quantity ratio relation respect Reynolds number right-hand side scalar shear stress shown shows solution tensor theory tion transport turbulence energy turbulence intensities turbulent flow turbulent motion turbulent region velocity correlation velocity distribution viscous sublayer vorticity wake flow wall region wavenumber wavenumber range zero