- Momentum thickness
In
aeronautics andviscous fluid theory , the boundary layer thickness () is the distance from a fixed boundary wall where zero flow is considered to occur, and beyond the fluid is considered to move at a constant velocity. This distance is calculated based on the total momentum of the fluid, rather than the total mass, as in the case ofdisplacement thickness (). The region of moving fluid contains a percentage (typically 97%) of the fluid's momentum, leading to the definition (fromincompressible fluid theory and thecontinuity equation ) mathematically, of::
The momentum thickness, θ, is a theoretical length scale to quantify the effects of fluid
viscosity in the vicinity of a physical boundary. Mathematically it is defined as:
(2.1)
where the vertical coordinate, z, is increasing upward from the boundary and uo is the velocity in the
ideal flow of the free stream. Thevelocity in a frictionalboundary layer is subject to theno-slip boundary condition at the surface (z = 0) and asymptotically approaches the free stream value (uo). Compared topotential flow , this would be the distance that the surface would be displaced for the flow to have the same momentum. The influence of fluidviscosity creates a wallshear stress , , which extracts energy from the mean flow. The boundary layer can be considered to possess a total momentum flux deficit,:
(2.2)
due to the frictional
dissipation . It may also be designated as δ2 as in Schlicting, H. (1979) Boundary-Layer Theory McGraw Hill, New York, U.S.A. 817 pp.For a flat plate at no
angle of attack with a laminar boundary layer, the Blasius solution gives:
(2.3)
Other length scales describing viscous boundary layers include the
boundary-layer thickness , ,displacement thickness , , andenergy thickness , .
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