Correction: Experiments on installed jet noise

Abstract

© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.Correction Notice Figure 9 caption should read: Acoustic spectra contour plot for the L/D= 3, r/D = 0.6 and ɑ = 0 deg jet/flat plate configuration, φ ≈ 0 deg (black curves) and 180 deg (blue curves), i.e. plate unshielded and shielded sides, respectively. Frames, from top to bottom: θ ≈ 90, 70, 50 and 30 deg. Frames, from left to right: Mach numbers of 0.4, 0.7 and 0.9. Acknowledgements should read: The authors would like to thank Ms. Barbara G. Hasparyk for her technical support with the assembling of the antenna, microphones calibration, writing the post-processing codes and many insightful conversations. We are also in debt with the Prométée plateforme technical staff and with Prof. JeanChristophe Robinet (DynFluid Laboratory). Part of this research was funded by Airbus and we thank Dr. Jérôme Hubert and Dr. Grégoire Pont for their inputs.