Receptivity of Boundary Layer over a Blunt Wedge due to Freestream Pulse Disturbances at Mach 6

<div>Instantaneous pressure disturbance in boundary layer for pulse wave.</div>

International Journal of Aerospace Engineering

Figure 3: Receptivity of Boundary Layer over a Blunt Wedge due to Freestream Pulse Disturbances at Mach 6 