Answer:
[tex]c_3_0_0_K=347.19m/s[/tex]
[tex]M=0.864[/tex]
Explanation:
The speed of sound in the air increases 0.6 m / s for every 1 ° C increase in temperature. An approximate speed can be calculated using the following empirical formula:
[tex]c=331.5+0.6\vartheta[/tex]
Where:
[tex]\vartheta=T-273.15K\\\\[/tex]
A more exact equation, usually referred to as adiabatic velocity of sound, is given by the following formula:
[tex]c=\sqrt{k*R*T}[/tex]
Where:
[tex]R= Gas\hspace{3}constant\hspace{3}of\hspace{3}air=0.287kJ/kg*K=287J/kg*K\\k=Specific\hspace{3}heat\hspace{3}ratio=1.4\\T=Temperature=300K[/tex]
Hence:
[tex]c=\sqrt{(287)*(1.4)*(300)} =347.1887095\approx347.19m/s[/tex]
Now, the Mach number at which an aircraft is flying can be calculated by:
[tex]M=\frac{u}{c}[/tex]
Where:
[tex]u= Velocity\hspace{3}of\hspace{3}the\hspace{3}moving\hspace{3}aircraft\\c= Speed\hspace{3}of\hspace{3}sound\hspace{3}at\hspace{3}the\hspace{3}given \hspace{3}altitude[/tex]
Therefore:
[tex]M=\frac{300}{347.19} =0.8640833984\approx0.864[/tex]