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Modern Engineering Thermodynamics

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16.4 The Mach Number 657<br />

Table 16.1 lists the jargon terms developed to describe the different flow regimes. Transonic flow is a flow in<br />

which the Mach number fluctuates around 1.0 by a small amount (±ε).<br />

We can deduce a relation for the dependence of the isentropic speed of sound (or sonic velocity) c on local thermodynamic<br />

properties from a mass and energy balance analysis of a moving acoustical wave. Figure 16.5 shows<br />

an open system attached to an isentropic sound wave moving at velocity c through a stationary fluid in a duct<br />

that has a constant cross-sectional area A. Our coordinate system is attached to the moving wave, so the fluid<br />

appears to be approaching the wave with velocity c. For an adiabatic, aergonic, reversible, steady state, steady<br />

flow, single-inlet, single-outlet open system, the mass rate balance (MRB) reduces to<br />

or<br />

_m in = _m out<br />

ρAc = ðρ + ∂ρ s ÞðAÞðc −∂V s Þ<br />

= Aðρc − ρ ∂V s + c ∂ρ s −∂ρ s ∂V s Þ<br />

Where the subscript s indicates that entropy is held constant during the differentiation process. Neglecting<br />

second-order differential terms (i.e., setting ∂ρ s ∂V s = 0), this equation can be rearranged to give<br />

<br />

∂V<br />

= c/ρ (16.6)<br />

∂ρ<br />

s<br />

Similarly, the energy rate balance for this system becomes<br />

h + c 2 /2g c = ðh + ∂h s Þ + ðc −∂V s Þ 2 /ð2g c Þ<br />

Again neglecting second-order differential terms, this can be expanded and rearranged to give<br />

<br />

∂h<br />

= c/g c (16.7)<br />

∂V s<br />

Finally, the Gibbs Eq. (7.21) for an isentropic process yields<br />

T∂s s = ∂h s − v∂p s = 0<br />

Table 16.1 Compressible Flow Mach Number Regimes (ε Is a Small Fluctuation)<br />

Flow Regime<br />

Name<br />

M < 1<br />

Subsonic<br />

M = 1<br />

Sonic<br />

1 − ε ≤ M ≤ 1 + ε Transonic<br />

M >1<br />

Supersonic<br />

M ≥ 5<br />

Hypersonic<br />

System boundary attached to a moving sound wave<br />

Upstream<br />

properties<br />

p<br />

ρ<br />

h<br />

and s<br />

Downstream<br />

properties<br />

c c − ∂ V s p + ∂p s<br />

ρ + ∂ρ s<br />

h + ∂ p s<br />

and s<br />

FIGURE 16.5<br />

An isentropic sound wave moving through a stationary fluid in a horizontal duct of constant cross-sectional area A. The coordinate<br />

system is fixed to the moving wave so that the surrounding fluid appears to be moving. The s subscript is used to indicate isentropic<br />

changes in the properties.

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