Sound radiation from airplane on the start

The problem of sound radiation from airplane during start on runway of aerodrome in wind action conditions is considered. The carriers of sound are aircraft engines, which are modeling in this paper by point sources moving in air with constant acceleration parallel to the plane interface of acoustic and solid elastic half-spaces. The solution of problem is obtained using the integral Fourier-transforms over time and space coordinates, and the stationary phase method. The numerical analysis of spatial-time distributions of instantaneous sound pressure and sound pressure level is carried out for a case of start of the two-engine airplane of Boeing 777-300ER type.