Sound production due to main-flow oriented vorticity-nozzle interaction in absence of a net swirl

L. Hirschberg, F. Bake, S. J. Hulshoff

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

Abstract

The downstream acoustic response due to the interaction of main-flow oriented vorticity with a choked nozzle in a swirl-free flow was experimentally demonstrated. The response was obtained by means of impulsive radial air injection in the pipe upstream from the nozzle. The resulting downstream acoustic data are shown to obey a scaling rule that differs, from the one for swirl-nozzle interaction, which according to the literature is proportional to the square of the swirl number. In contrast, here evidence is presented that points to the scaling of main-flow oriented vorticity noise with the cross-sectional average of the square of the transversal velocity at the throat divided by the square of the critical sound speed.

Original languageEnglish
Title of host publication28th AIAA/CEAS Aeroacoustics Conference, 2022
PublisherAmerican Institute of Aeronautics and Astronautics
ISBN (Print)9781624106644
DOIs
Publication statusPublished - 2022
Externally publishedYes
Event28th AIAA/CEAS Aeroacoustics Conference 2022 - Southampton, United Kingdom
Duration: 14 Jun 202217 Jun 2022
Conference number: 28

Conference

Conference28th AIAA/CEAS Aeroacoustics Conference 2022
Country/TerritoryUnited Kingdom
CitySouthampton
Period14/06/2217/06/22

Keywords

  • n/a OA procedure

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