Aeroacoustic fields of supersonic twin jets at the ideally expanded condition

Yuta Ozawa, Taku Nonomura, Yuji Saito, Keisuke Asai

Research output: Contribution to journalArticlepeer-review

Abstract

The aeroacoustic fields of twin jets and the equivalent single jet were experimentally investigated using particle image velocimetry (PIV), schlieren visualization, and acoustic measurement. The present study focuses on the aeroacoustic fields of the twin jets, and the effect of the interaction between each jet was investigated using various nozzle spacing. The PIV results indicated that strong interaction causes elliptical jet growth on a cross-stream plane and a decrease in the Reynolds stress of the inner shear layer on a plane containing both jet axes. The dynamic mode decomposition of the double-pulsed schlieren images extracted the interaction of each jet, which relates to the Mach wave generation. The noise of the twin jets was basically quieter than the noise of an equivalent single jet because of a shielding effect and a reduction in the Reynolds stress resulting in a decrease in the overall sound pressure level.

Original languageEnglish
Pages (from-to)312-324
Number of pages13
JournalTransactions of the Japan Society for Aeronautical and Space Sciences
Volume64
Issue number6
DOIs
Publication statusPublished - 2021

Keywords

  • Aeroacoustics
  • Supersonic Jet
  • Twin Jets

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

Fingerprint

Dive into the research topics of 'Aeroacoustic fields of supersonic twin jets at the ideally expanded condition'. Together they form a unique fingerprint.

Cite this