Simulation of Instabilities and Sound Radiation in a Jet

Alvin Bayliss, Lucio Maestrello

Research output: Contribution to journalArticlepeer-review

16 Scopus citations

Abstract

The inflow and near field of a jet that is excited by an axial mass source located in the potential core are simulated numerically. The simulation takes into account the spreading of the jet. Comparison is made with experimental results for both excited and unexcited jets. It is shown that many of the features observed experimentally are due to the instability of the mean profile (i.e., the large-scale structures) and not due to the turbulence. The instability is shown to generate low-frequency sound. The terms identified by Ribner as the shear noise terms are shown to be responsible for this sound generation.

Original languageEnglish (US)
Pages (from-to)835-841
Number of pages7
JournalAIAA journal
Volume19
Issue number7
DOIs
StatePublished - Jul 1981

Funding

This work was partially supported under NASA Contracts No. NAS1-14472 and NAS1-15810 while the first author was in residence at the Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, Hampton, Va., 23665. Additional support for the first author was provided by Air Force Contract No. AFOSR-76-2881.

ASJC Scopus subject areas

  • Aerospace Engineering

Fingerprint

Dive into the research topics of 'Simulation of Instabilities and Sound Radiation in a Jet'. Together they form a unique fingerprint.

Cite this