The inflight acoustic characteristics of high velocity jet noise suppressor nozzles for supersonic cruise aircraft were reviewed. The inflight effects at the peak noise level were discussed. Both single and inverted velocity profile multistream suppressor nozzles were considered. The importance of static spectral shape on the noise reduction due to inflight effects was stressed.
Acoustic considerations of flight effects on jet noise suppressor nozzles
AIAA 18th Aerospace Sci. Meeting ; 1980 ; Pasadena, CA, United States
1979-01-01
Conference paper
No indication
English