Question

If a supersonic jet flies at Mach 3.2, what will be the cone angle (to the nearest degree)?

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We will use the formula:

sinθ2=SsSa(1)\begin{align*} \textcolor{#4257b2}{\sin\dfrac{\theta}{2}=\dfrac{S_s}{S_a}\quad\quad (1)} \end{align*}

where SaS_a is the speed of the aircraft, SsS_s is the speed of sound and θ\theta is the angle of the sound cone.

We are given:

Sb=Mach 3.2\begin{align*} S_b&=\text{Mach }3.2 \end{align*}

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