Calculating Shear Stress: Solving for μ = ρv in 8-41 Equation

AI Thread Summary
The discussion focuses on the confusion surrounding the equation μ = ρv, particularly regarding the units of viscosity (μ) and the product of density (ρ) and velocity (v). Participants clarify that the lowercase 'v' represents velocity, while the Greek letter nu (ν) denotes kinematic viscosity, defined as ν = μ/ρ. The conversation also addresses how to derive the formula for the viscous sublayer by substituting u = √(τ/ρ) into equation 8-41 and rearranging it to match the form of equation 8-42. Additionally, there are corrections regarding mathematical cancellations that the original poster misapplied. Understanding these distinctions and corrections is crucial for solving the problem accurately.
hotjohn
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Homework Statement


how to make μ = ρ v as in 8-41 ?

Homework Equations

The Attempt at a Solution


since μ = viscocity , it has unit =( kgms^-2)s m^-2 , = kg(m^-1)(s^-1)
ρ v = (kgm^-3)(ms^-1 ) = kg(m^-2)(s^-1) , the unit for LHS and RHS are not the same , can someone help pls ?
 

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hotjohn said:

Homework Statement


how to make μ = ρ v as in 8-41 ?

Homework Equations

The Attempt at a Solution


since μ = viscocity , it has unit =( kgms^-2)s m^-2 , = kg(m^-1)(s^-1)
ρ v = (kgm^-3)(ms^-1 ) = kg(m^-2)(s^-1) , the unit for LHS and RHS are not the same , can someone help pls ?
You've mixed up lower case v for velocity with the lower case Greek letter nu (##\nu##), which is used to represent the kinematic viscosity of a fluid.

The kinematic viscosity is defined ##\nu = \frac{\mu}{\rho}##

See this article for a discussion of the units:

https://en.wikipedia.org/wiki/Viscosity
 
SteamKing said:
You've mixed up lower case v for velocity with the lower case Greek letter nu (##\nu##), which is used to represent the kinematic viscosity of a fluid.

The kinematic viscosity is defined ##\nu = \frac{\mu}{\rho}##

See this article for a discussion of the units:

https://en.wikipedia.org/wiki/Viscosity
ok , can you pls explain how the author get the formula of viscous sublayer ? after substitute u= sqrt rt (τ / ρ ) into 8-41 , I have u = ( v / y ) sqrt rt (τ / ρ ) , hwo to get the same form as in 8-42 ?
 

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Note that ##\sqrt{\tau_w/\rho}## is defined to be a fictitious velocity ##u##- (called "friction velocity"). (I'm not sure I got the notation right. It looks like there is a subscript "-" on the ##u## for the fictitious velocity. But it is hard for me to read.) See discussion below equation 8-41.
##u##- is not the same as the actual velocity ##u##.
 
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TSny said:
Note that ##\sqrt{\tau_w/\rho}## is defined to be the "fictitious velocity" ##u##-. (I'm not sure I got the notation right. It looks like there is a subscript "-" on the ##u## for the fictitious velocity. But it is hard for me to read.) See discussion below equation 8-41.
##u##- is not the same as the actual velocity ##u##.
u / ##u##- , i haver u [ sqrt rt ( p / т ) ] , how to get the same form as in the 8-42 ?
 
Solve ##u##- = ##\sqrt{\tau/\rho}## for ##\tau##. Then sustitute this expression for ##\tau## into equation 8-41. You should then be able to rearrange it to get 8-42.
 
TSny said:
Solve ##u##- = ##\sqrt{\tau/\rho}## for ##\tau##. Then sustitute this expression for ##\tau## into equation 8-41. You should then be able to rearrange it to get 8-42.
hwo to do that ? I have tried , but didn't get the same form ,
 

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hotjohn said:
hwo to do that ? I have tried , but didn't get the same form ,
Some of your cancellations are wrong. ##\frac x{\sqrt x}## is not ##\frac 1{\sqrt x}##
 
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