Research Article

Response of a Hypersonic Boundary Layer to Freestream Pulse Acoustic Disturbance

Figure 8

Fourier frequency analysis of pressure disturbance at different surface locations under freestream pulse fast acoustic wave.
748504.fig.008a
(a)
748504.fig.008b
(b)
748504.fig.008c
(c)
748504.fig.008d
(d)
748504.fig.008e
(e)
748504.fig.008f
(f)