Effects of nozzle-exit boundary-layer profile on the initial shear-layer instability, flow field and noise of subsonic jets
Work
Year: 2019
Type: article
Abstract: The influence of the nozzle-exit boundary-layer profile on high-subsonic jets is investigated by performing compressible large-eddy simulations (LES) for three isothermal jets at a Mach number of 0.9 ... more
Source: Journal of Fluid Mechanics
Authors Christophe Bogey, Roberto Sabatini
Institutions Laboratoire de Mécanique des Fluides et d'Acoustique, Embry–Riddle Aeronautical University
Cites: 106
Cited by: 41
Related to: 10
FWCI: 4.273
Citation percentile (by year/subfield): 100
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: green