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Basics of Fluid Mechanics, 2014a

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320 CHAPTER 9. DIMENSIONAL ANALYSIS<br />

For the Continuity Equation (8.17) for non–compressible substance can be transformed<br />

into<br />

0<br />

∂ρ<br />

✁∂t ✁✁✕ + ∇·(˜ρ U) =0 (9.51)<br />

For the N-S equation, every additive term has primary dimensions m 1 L −2 t −2 .<br />

To non nondimensionalization, we multiply every term by L/(V 2 ), which has primary<br />

dimensions m −1 L 2 t 2 , so that the dimensions cancel.<br />

Using these definitions equation (8.111) results in<br />

fh ∂ŨU<br />

( )<br />

(ŨU<br />

U 0 ∂˜t + · ˜∇<br />

Pmax − P ∞<br />

)ŨU = −<br />

˜∇ ˜P<br />

ρŨU<br />

+ 1 ⃗f<br />

ŨU 2 g + 1 ˜∇ 2<br />

ρŨU ŨU (9.52)<br />

h<br />

gh μ<br />

Or after using the definition <strong>of</strong> the dimensionless parameters as<br />

St ∂ŨU (ŨU<br />

∂˜t + · ˜∇<br />

)ŨU = −Eu ˜∇ ˜P + 1<br />

Fr ⃗ 2 f g + 1 Re ˜∇ 2 ŨU (9.53)<br />

The definition <strong>of</strong> Froude number is not consistent in the literature. In some places Fr<br />

is defined as the square <strong>of</strong> Fr = U 2 /g h.<br />

The Strouhal number is named after Vincenz Strouhal (1850 1922), who used<br />

this parameter in his study <strong>of</strong> “singing wires.” This parameter is important in unsteady,<br />

oscillating flow problems in which the frequency <strong>of</strong> the oscillation is important.<br />

Example 9.23:<br />

A device is accelerated linearly by a constant value B. Write a new N–S and continuity<br />

equations for incompressible substance in the a coordinate system attached to the body.<br />

Using these equations developed new dimensionless equations so the new “Froude number”<br />

will contain or “swallow” by the new acceleration. Measurement has shown that<br />

the acceleration to be constant with small sinusoidal on top the constant such away as<br />

( ) f<br />

a = B + ɛ sin<br />

(9.XXIII.a)<br />

2 π<br />

Suggest a dimensionless parameter that will take this change into account.<br />

Supplemental Problems<br />

1. An airplane wing <strong>of</strong> chord length 3 [m] moves through still air at 15 ◦ Cand 1 [Bar]<br />

and at at a speed <strong>of</strong> 15 [m/sec]. What is the air velocity for a 1:20 scale model<br />

to achieve dynamic similarity between model and prototype? Assume that in the<br />

model the air has the same pressure and temperature as that in prototype. If the<br />

air is considered as compressible, what velocity is required for pressure is 1.5[bar]<br />

and temperature 20 ◦ C? What is the required velocity <strong>of</strong> the air in the model test<br />

when the medium is made <strong>of</strong> water to keep the dynamic similarity?

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