Shear velocity

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Shear Velocity, also called friction velocity, is a form by which a shear stress may be re-written in units of velocity. It is useful as a method in fluid mechanics to compare true velocities, such as the velocity of a flow in a stream, to a velocity that relates shear between layers of flow.


Shear velocity is used to describe shear-related motion in moving fluids. It is used to describe:




  • Diffusion and dispersion of particles, tracers, and contaminants in fluid flows

  • The velocity profile near the boundary of a flow (see Law of the wall)

  • Transport of sediment in a channel


Shear velocity also helps in thinking about the rate of shear and dispersion in a flow. Shear velocity scales well to rates of dispersion and bedload sediment transport. A general rule is that the shear velocity is between 5% to 10% of the mean flow velocity.


For river base case, the shear velocity can be calculated by Manning's equation.


u∗=⟨u⟩na(gRh−1/3)0.5{displaystyle u^{*}=langle urangle {frac {n}{a}}(gR_{h}^{-1/3})^{0.5}}{displaystyle u^{*}=langle urangle {frac {n}{a}}(gR_{h}^{-1/3})^{0.5}}



  • n is the Gauckler–Manning coefficient. Units for values of n are often left off, however it is not dimensionless, having units of: (T/[L1/3]; s/[ft1/3]; s/[m1/3]).


  • Rh is the hydraulic radius (L; ft, m);

  • the role of a is a dimension correct factor. Thus a= 1 m1/3/s = 1.49 ft1/3/s.


Instead of finding n{displaystyle n}n and Rh{displaystyle R_{h}}{displaystyle R_{h}} for your specific river of interest, you can examine the range of possible values and note that for most rivers, u∗{displaystyle u^{*}}u^{*} is between 5% and 10% of u⟩{displaystyle langle urangle }{displaystyle langle urangle }:


For general case


u⋆ρ{displaystyle u_{star }={sqrt {frac {tau }{rho }}}}u_{{star }}={sqrt  {{frac  {tau }{rho }}}}

where τ is the shear stress in an arbitrary layer of fluid and ρ is the density of the fluid.


Typically, for sediment transport applications, the shear velocity is evaluated at the lower boundary of an open channel:


u⋆{displaystyle u_{star }={sqrt {frac {tau _{b}}{rho }}}}u_{{star }}={sqrt  {{frac  {tau _{b}}{rho }}}}

where τb is the shear stress given at the boundary.


Shear velocity can also be defined in terms of the local velocity and shear stress fields (as opposed to whole-channel values, as given above).



Friction Velocity in Turbulence


The friction velocity is often used as a scaling parameter for the fluctuating component of velocity in turbulent flows.[1] One method of obtaining the shear velocity is through non-dimensionalization of the turbulent equations of motion. For example, in a fully developed turbulent channel flow or turbulent boundary layer, the streamwise momentum equation in the very near wall region reduces to:



0=ν2u¯y2−y(u′v′¯){displaystyle 0={nu }{partial ^{2}{overline {u}} over partial y^{2}}-{frac {partial }{partial y}}({overline {u'v'}})}0={nu }{partial ^{2}overline {u} over partial y^{2}}-{frac  {partial }{partial y}}(overline {u'v'}).

By integrating in the y-direction once, then non-dimensionalizing with an unknown velocity scale u and viscous length scale ν/u, the equation reduces down to:


τu∂y−u′v′¯{displaystyle {frac {tau _{w}}{rho }}=nu {frac {partial u}{partial y}}-{overline {u'v'}}}{frac  {tau _{w}}{rho }}=nu {frac  {partial u}{partial y}}-overline {u'v'}

or



τu⋆2=∂u+∂y++τT+¯{displaystyle {frac {tau _{w}}{rho u_{star }^{2}}}={frac {partial u^{+}}{partial y^{+}}}+{overline {tau _{T}^{+}}}}{frac  {tau _{w}}{rho u_{{star }}^{2}}}={frac  {partial u^{+}}{partial y^{+}}}+overline {tau _{T}^{+}}.

Since the right hand side is in non-dimensional variables, they must be of order 1. This results in the left hand side also being of order one, which in turn give us a velocity scale for the turbulent fluctuations (as seen above):



u⋆{displaystyle u_{star }={sqrt {frac {tau _{w}}{rho }}}}u_{{star }}={sqrt  {{frac  {tau _{w}}{rho }}}}.

Here, τw refers to the local shear stress at the wall.





Planetary boundary layer


Within the lowest portion of the planetary boundary layer a semi-empirical log wind profile is commonly used to describe the vertical distribution of horizontal mean wind speeds.
The simplified equation that describe it is



u(z)=u∗κ[ln⁡(z−dz0)]{displaystyle u(z)={frac {u_{*}}{kappa }}left[ln left({frac {z-d}{z_{0}}}right)right]}{displaystyle u(z)={frac {u_{*}}{kappa }}left[ln left({frac {z-d}{z_{0}}}right)right]}



where κ{displaystyle kappa }kappa is the Von Kármán constant (~0.41), d{displaystyle d}d is the zero plane displacement (in metres).


The zero-plane displacement (d{displaystyle d}d) is the height in meters above the ground at which zero wind speed is achieved as a result of flow obstacles such as trees or buildings. It can be approximated as 2/3 to 3/4 of the average height of the obstacles.[2] For example, if estimating winds over a forest canopy of height 30 m, the zero-plane displacement could be estimated as d = 20 m.


Thus, you can extract the friction velocity by knowing the wind velocity at two levels (z).



u∗(u(z2)−u(z1))ln⁡(z2−dz1−d){displaystyle u_{*}={frac {kappa (u(z2)-u(z1))}{ln left({frac {z2-d}{z1-d}}right)}}}{displaystyle u_{*}={frac {kappa (u(z2)-u(z1))}{ln left({frac {z2-d}{z1-d}}right)}}}




References





  1. ^ Schlichting, H.; Gersten, K. Boundary-Layer Theory (8th ed.). Springer 1999. ISBN 978-81-8128-121-0..mw-parser-output cite.citation{font-style:inherit}.mw-parser-output .citation q{quotes:"""""""'""'"}.mw-parser-output .citation .cs1-lock-free a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/6/65/Lock-green.svg/9px-Lock-green.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .citation .cs1-lock-limited a,.mw-parser-output .citation .cs1-lock-registration a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/d/d6/Lock-gray-alt-2.svg/9px-Lock-gray-alt-2.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .citation .cs1-lock-subscription a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/a/aa/Lock-red-alt-2.svg/9px-Lock-red-alt-2.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registration{color:#555}.mw-parser-output .cs1-subscription span,.mw-parser-output .cs1-registration span{border-bottom:1px dotted;cursor:help}.mw-parser-output .cs1-ws-icon a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/4/4c/Wikisource-logo.svg/12px-Wikisource-logo.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output code.cs1-code{color:inherit;background:inherit;border:inherit;padding:inherit}.mw-parser-output .cs1-hidden-error{display:none;font-size:100%}.mw-parser-output .cs1-visible-error{font-size:100%}.mw-parser-output .cs1-maint{display:none;color:#33aa33;margin-left:0.3em}.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registration,.mw-parser-output .cs1-format{font-size:95%}.mw-parser-output .cs1-kern-left,.mw-parser-output .cs1-kern-wl-left{padding-left:0.2em}.mw-parser-output .cs1-kern-right,.mw-parser-output .cs1-kern-wl-right{padding-right:0.2em}


  2. ^ Holmes JD. Wind Loading of Structures. 3rd ed. Boca Raton, Florida: CRC Press; 2015.




  • Whipple, K. X. (2004). "III: Flow Around Bends: Meander Evolution" (PDF). MIT. 12.163 Course Notes.



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