The ratio of static pressure after a normal shockwave to before the shockwave is 9.986. Determine the Mach number of the aircraft.

Respuesta :

The Mach number of aircraft is 2.95.

The equation to be used in case of normal shockwave is -

p₁/p₀= 2γM-(γ-1)/(γ+1)

where, γ represents specific heat ratio which is 1.4, p₁/p₀ represents ratio of static pressure after a normal shockwave to before the shockwave, M is Mach number.

Now, keeping the values in formula to find the Mach number.

[tex]9.986 = \frac{2*1.4*M^{2} - (1.4-1) }{(1.4+1)}[/tex]

Performing addition in denominator to find the value of Mach number

[tex]9.986 = \frac{2*1.4*M^{2} - (1.4-1) }{(2.4)}[/tex]

Performing subtraction on Right Hand Side

[tex]9.986*2.4 = 2.8*M^{2} -0.4[/tex]

Performing multiplication on Left Hand Side to find the value of Mach number

[tex]23.97 = 2.8*M^{2} - 0.4[/tex]

Shifting value from Left Hand Side to Right Hand Side

[tex]23.97 + 0.4 = 2.8*M^{2}[/tex]

Performing addition on Left Hand Side to find the value of Mach number

[tex]24.37 = 2.8*M^{2}[/tex]

[tex]M^{2} = \frac{24.37}{2.8}[/tex]

Performing division to find the value of Mach number

[tex]M^{2} = 8.7[/tex]

[tex]M = \sqrt{8.7}[/tex]

Taking square root to calculate the final answer

[tex]M = 2.95[/tex]

Hence, the Mach number is 2.95.

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