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Basics of Fluid Mechanics, 2014a

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240 CHAPTER 8. DIFFERENTIAL ANALYSIS<br />

Equation (8.30) can be further rearranged so derivative <strong>of</strong> the density is equal the<br />

divergence <strong>of</strong> velocity as<br />

( substantial derivative<br />

{ }} { )<br />

1 ∂ρ<br />

ρ ∂t + U ∇·ρ = −∇ · U (8.31)<br />

Equation (8.31) relates the density rate <strong>of</strong> change or the volumetric change to the<br />

velocity divergence <strong>of</strong> the flow field. The term in the bracket LHS is referred in the<br />

literature as substantial derivative. The substantial derivative represents the change<br />

rate <strong>of</strong> the density at a point which moves with the fluid.<br />

Acceleration Direct Derivations<br />

One <strong>of</strong> the important points is to find the fluid particles acceleration. A fluid<br />

particle velocity is a function <strong>of</strong> the location and time. Therefore, it can be written that<br />

U(x, y, z, t) =U x (x, y, x, t) î + U y (x, y, z, t) ĵ + U z (x, y, z, t) ̂k (8.32)<br />

Therefor the acceleration will be<br />

DU<br />

Dt = dU x<br />

dt î + dU y<br />

ĵ + dU z ̂k (8.33)<br />

dt dt<br />

The velocity components are a function <strong>of</strong> four variables, (x, y, z, and t), and hence<br />

DU x<br />

Dt<br />

= ∂U x<br />

∂t<br />

=1<br />

{}}{<br />

dt<br />

dt +∂U x<br />

∂x<br />

The acceleration in the x can be written as<br />

U {}}{<br />

x<br />

dx<br />

dt +∂U x<br />

∂y<br />

U y<br />

{}}{<br />

dy<br />

dt +∂U x<br />

∂z<br />

U z<br />

{}}{<br />

dz<br />

dt<br />

(8.34)<br />

DU x<br />

Dt<br />

= ∂U x<br />

∂t<br />

∂U x<br />

+ U x<br />

∂x + U ∂U x<br />

y<br />

∂y<br />

+ U ∂U x<br />

z<br />

∂z<br />

= ∂U x<br />

+(U ·∇) U x (8.35)<br />

∂t<br />

The same can be developed to the other two coordinates which can be combined (in a<br />

vector form) as<br />

dU<br />

dt = ∂U<br />

∂t +(U ·∇) U (8.36)<br />

or in a more explicit form as<br />

local<br />

acceleration<br />

convective<br />

acceleration<br />

{}}{ { }} {<br />

dU<br />

dt = ∂U<br />

+ U ∂U<br />

∂t ∂x + U ∂U<br />

∂y + U ∂U<br />

(8.37)<br />

∂z<br />

The time derivative referred in the literature as the local acceleration which vanishes<br />

when the flow is in a steady state. While the flow is in a steady state there is only<br />

convective acceleration <strong>of</strong> the flow. The flow in a nozzle is an example to flow at<br />

steady state but yet has acceleration which flow with a very low velocity can achieve a<br />

supersonic flow.

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