The application discloses a kind of hypersonic speed cavity flow induced
noise passive control device and control method, it is suitable for Mach number 4.0 flow M219 classic
open cavity, its size is normalized with the cavity depth as benchmark, cavity length-width-depth ratio 5:1:1, at the bottom of cavity downstream, from the front wall, setting integrated three-dimensional small-size continuous triangular
pyramid turbulence device, length-width-height size is,, Using
aviation titanium alloy or high-temperature
alloy;The installation position is determined by IDDES
simulation, the scale of downstream
backflow vortex is reduced by using turbulence structure, the
impact of bottom wall is weakened, self-sustaining oscillation is inhibited, the
peak value of Rossiter low-frequency mode is reduced, and the maximum total
sound pressure level is reduced by about 4dB.The application is pure
passive control, without additional
energy consumption, simple structure, suitable for
noise suppression of cavity structure such as internal embedded bomb cabin of hypersonic vehicle.