Receptivity and Forced Response to Acoustic Disturbances in High-Speed Boundary Layers
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Supersonic boundary-layer receptivity to freestream acoustic disturbances is investigated by solving the Navier-Stokes equations for Mach 3.5 flow over a 7 deg half-angle cone. The freestream disturbances are generated from a wavy wall placed at the nozzle wal... ...
