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Chapter 3: Some Fundamental Aspects of Compressible Flow



Problem 3.17:

An observer on the ground finds that an airplane flying horizontally at an altitude of m has traveled km from the overhead position before the sound of the airplane is first heard. Assuming that, overall, the aircraft creates a small disturbance, estimate the speed at which the airplane is flying. The average air temperature between the ground and the altitude at which the airplane is flying is oC. Explain the assumptions you have made in arriving at the answer.

Solution:

Given:
altitude = 2500 m,
distance travelled = 6 km,
\( T_{\text{avg}} = \) 10oC = 283 K.

To calculate: \( V=? \)

The problem description is schematically shown in Fig. 1.

Fig. 1: Schematic of the problem description

Using trigonometric relation we can estimate the Mach angle as,

\[ \tan\mu=\frac{\text{altitude}}{\text{distance}}=\frac{2500}{6000}\ \implies\ \mu=\tan^{-1}\left(\frac{2.5}{6}\right) \]

The Mach angle is defined in terms of Mach number as,

\[ \sin\mu=\frac{1}{M}\ \implies\ M=\frac{1}{\sin\mu} \]
\[ M=\frac{1}{\sin\left(\tan^{-1}\left(2.5/6\right)\right)} \]
\[ M=2.6\ . \]

The velocity can be calculated as,

\[ V=M\,a \]
\[ V=M\,\sqrt{\gamma\,R\,T_{\text{avg}}}=2.6\times\sqrt{1.4\times287\times283} \]
\[ \boxed{V=876.74\,\text{m/s}}\ . \]



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