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 language | English (US) |
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Pages (from-to) | 835-841 |
Number of pages | 7 |
Journal | AIAA journal |
Volume | 19 |
Issue number | 7 |
DOIs | |
State | Published - 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