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Chapter 3: Some Fundamental Aspects of Compressible Flow



Problem 3.12:

A gas with a molar mass of and a specific heat ratio flows through a channel at supersonic speed. The temperature of the gas in the channel is oC. A photograph of the flow reveals weak waves originating at imperfections in the wall running across the flow at an angle to o to the flow direction. Find the Mach number and the velocity in the flow.

Solution:

Given:
\( \hat{m} =\) 44 kg/kmol,
\( \gamma = \) 1.67,
\( T = \) 10oC = 283 K,
Mach angle = \( \mu = \) 45o.

To calculate: \( M=?, V=? \)

The problem description is schematically shown in Fig. 1.

Fig. 1: Schematic of the problem description

The Mach angle is given by the equation,

\[ \sin\left(\mu\right)=\frac{1}{M} \]
\[ M=\frac{1}{\sin\left(\mu\right)}=\frac{1}{\sin\left(45\right)} \]
\[ \boxed{M=1.4142}\ . \]

The speed of sound in the channel, for the given temperature, can be calculated as,

\[ a=\sqrt{\gamma\,R\,T} \]

where, the value of gas constant $R$ can be calculated as,

\[ R=\frac{R_{u}}{\hat{m}} \]

therefore,

\[ a=\sqrt{\gamma\,\frac{R_{u}}{\hat{m}}\,T} \]

The velocity can be calculated, using the universal gas constant \( R_{u}= \) 8314 J/kmol-K and the given molar mass of the gas \( \hat{m} =\) 44 kg/kmol,

as,
\[ V=M\,a=\frac{1}{\sin\left(\mu\right)}\times\sqrt{\gamma\,\frac{R_{u}}{\hat{m}}\,T}=\frac{1}{\sin\left(45\right)}\times\sqrt{1.67\times\frac{8314}{44}\times283} \]
\[ \boxed{V=422.6152\,\text{m/s}}\ . \]



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