Why do the units not match for μ = ρv?

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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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  • Textbook page on turbulent velocity profile: a figure of laminar and turbulent pipe velocity profiles with labeled layers, followed by explanatory text and equations for shear stress and friction velocity.
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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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  • Textbook page on turbulent pipe flow showing equations 8-42 to 8-47 for the viscous sublayer, law of the wall, and logarithmic velocity profile, with a log-scale graph of Eq. 8-42, Eq. 8-47 and experimental data labelled Figure 8-25.
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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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  • Handwritten algebra on lined paper: y/u_w = (τn y / (P v)) / sqrt(τn / P), then = (τn y / (P v)) times (sqrt(P) / sqrt(τn)), then = sqrt(P) y / (sqrt(τn) v).
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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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