ON THE STRUCTURE OF THE SOUND FIELD NEAR A TURBULENT JET EMANATING FROM A NOZZLE IN THE CASE WHERE PERTURBATIONS EXIST IN ITS PRECHAMBER

Results of investigation of the structure of the sound fi eld near a supersonic isothermal air jet emanating from the nozzle of a jet engine under the conditions of existence of perturbations in its jet-edge generator by the direct shadow method are presented.
Results of investigation of the structure of the sound fi eld near a supersonic isothermal air jet emanating from the nozzle of a jet engine under the conditions of existence of perturbations in its jet-edge generator by the direct shadow method are presented.
Author:  V. G. Pimshtein
Keywords:  Results of investigation of the structure of the sound fi eld near a supersonic isothermal air jet emanating from the nozzle of a jet engine under the conditions of existence of perturbations in its jet-edge generator by the direct shadow method are presented.
Page:  666-668