Response of a Hypersonic Boundary Layer to Freestream Pulse Acoustic Disturbance

Table 1

Computational conditions.

Re	Ma∞	𝑇∞ (K)	𝑇𝑤 (K)	𝛼𝑛 (°)	𝑅 (mm)	𝜃 (°)
10000	6	169	200	0	1	8