Aerospace Lab is an electronic journal dedicated to scientific progress in aeronautics and space research. Its featured technical fields therefore include aerodynamics, propulsion, materials, structures, physics, sensors, information processing, and system engineering.
An analysis of shock noise components
Auteurs:
C. Bailly, B. André, T. Castelain (Université de Lyon)
C. Henry, G. Bodard (Snecma)
M. Porta (Airbus)
| Attachment | Size |
|---|---|
 AL07-06_0.pdf | 2.26 MB |
Screech and broadband shock-associated noise linked to the presence of a shockcell structure in supersonic jets are reviewed in this paper. Only underexpanded supersonic circular jets issued from a convergent nozzle are considered here. An overview of the flow and of these two noise components is presented, based on recent experimental and numerical work. Flight effects on broadband shock-associated noise are also introduced, within the framework of aeronautical applications.
