Response of a Hypersonic Boundary Layer to Freestream Pulse Acoustic Disturbance

Figure 5

Contours of pressure 𝑃^′(𝑥,𝑦,𝑡), density 𝜌^′(𝑥,𝑦,𝑡), temperature 𝑇^′(𝑥,𝑦,𝑡), and velocity disturbance.

(a)

(b)

(c)

(d)