Shock waves in supersonic jets and aeroacoustic couplings – JESSICA
JESSICA - Shock waves in supersonic jets and aeroacoustic couplings. Prediction and control of pressure fluctuations induced by shock-cell structures in turbulent shear flows are currently facing a challenge, imperfectly expanded jets occuring in many practical systems. Two distinct applications in various industrial fields, namely aerospace and energy, are directly involved in this project, which involves research teams using similar analytical, numerical and experimental approaches: the Laboratoire de Mécanique des Fluides et d’Acoustique (LMFA UMR CNRS 5509), the Institut PPRIMME (UPR CNRS 3346) and the Laboratoire de Mécanique des Structures Industrielles Durables (LaMSID, UMR CNRS-EDF 2832).
Project coordination
Christophe Bailly (ECOLE CENTRALE DE LYON) – christophe.bailly@ec-lyon.fr
The author of this summary is the project coordinator, who is responsible for the content of this summary. The ANR declines any responsibility as for its contents.
Partner
LMFA UMR CNRS 5509 ECOLE CENTRALE DE LYON
UPR CNRS 3346 CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE - DELEGATION REGIONALE CENTRE POITOU-CHARENTES
LaMSID UMR CNRS-EDF 2832 CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE - DELEGATION REGIONALE ILE-DE-FRANCE SECTEUR OUEST ET NORD
Help of the ANR 399,924 euros
Beginning and duration of the scientific project:
- 36 Months
