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Flow and Acoustic Fields of Rocket Jets Impinging on a Perforated Plate

Mathieu Varé

https://orcid.org/0000-0002-8315-7470

Laboratoire de Mécanique des Fluides et d'Acoustique, LMFA UMR 5509, 69130 Ecully, France

*Postdoctoral Fellow; .

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and

Christophe Bogey

https://orcid.org/0000-0003-3243-747X

Laboratoire de Mécanique des Fluides et d'Acoustique, LMFA UMR 5509, 69130 Ecully, France

†CNRS Research Scientist; . Associate Fellow AIAA.

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Published Online:10 Apr 2022https://doi.org/10.2514/1.J061253

Abstract

The flow and acoustic fields of jets at a Mach number of 3.1 impinging on a plate at $15 D$ of the jet nozzle exit, where $D$ is the nozzle diameter, have been investigated using highly resolved large-eddy simulations. The plate is perforated with a hole of diameter $h = 1.33 D$ , $2 D$ , $3 D$ , or $4 D$ . The full-plate and free-jet cases have also been considered. The pressure levels are highest for the non-perforated plate and decrease as the hole diameter increases. Compared with the free jet, they are higher by about 5 dB for the full plate, 4 dB for $h = 1.33 D$ and $2 D$ , 3 dB for $h = 3 D$ , and 2 dB for $h = 4 D$ . In the upstream direction, the broadband shock-associated noise is prevailing for the free jet. For the impinging jets, the main noise component in that direction is produced by the impingement of the jet turbulent structures on the plate. In the downstream direction, for the free jet and down to the plate for the impinging jets, the sound field is dominated by Mach waves. Downstream of the perforated plates, waves are generated by interactions between the jet flow and the plate.

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Volume 60, Number 8August 2022

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Copyright © 2022 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.

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Acknowledgments

This work was financed by ArianeGroup and the Direction Générale de l’Armement (DGA). It was also financially supported by the IRICE IJES project RA0014963 (Installed Jet Effect Simulator, FEDER-FSE Rhône-Alpes). It was granted access to the HPC resources of Pôle de Modélisation et de Calcul en Sciences de l’Ingénieur et de l’Information (PMCS2I) of Ecole Centrale de Lyon, Pôle Scientifique de Modélisation Numérique (PSMN) of ENS de Lyon, members of Fédération Lyonnaise de Modélisation et Sciences Numériques (FLMSN), partner of EQUIPEX [email protected], and to the resources of Institut du Développement et des Ressources en Informatique Scientifique (IDRIS) under the allocation 2021-2a0204 made by Grand Equipement National de Calcul Intensif (GENCI). It was performed within the framework of the LABEX CeLyA (ANR-10-LABX-0060) of Université de Lyon, within the program Investissements d’Avenir (ANR-16-IDEX-0005) operated by the French National Research Agency (ANR). The authors also gratefully acknowledge the Centre National d’Études Spatiales (CNES) for sharing the data of the MARTEL experiments.

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Received3 September 2021
Accepted22 February 2022
Published online10 April 2022

Flow and Acoustic Fields of Rocket Jets Impinging on a Perforated Plate

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