The resonance of twin supersonic jets
Abstract
This paper presents an analytical study of the resonant interaction between twin supersonic jets. An instability wave model is used to describe the large scale coherent structures in the jet mixing layers. A linearized shock cell model is also given for the jets when operating off design. The problem's geometry admits four types of normal modes associated with each azimuthal mode number in the single jet. The stability of these modes is examined for both a vortex sheet model of the jet and a jet flow represented by realistic profiles. The growth rates of each mode number and type are found to vary with jet separation and mixing layer thickness and Strouhal number. Contours of equal pressure level are obtained for each mode. The region close to the symmetry axis is found to have the greatest pressure fluctuation amplitude.
- Publication:
-
American Institute of Aeronautics and Astronautics Conference
- Pub Date:
- April 1989
- Bibcode:
- 1989aiaa.confR....M
- Keywords:
-
- Aeroacoustics;
- Interactional Aerodynamics;
- Jet Mixing Flow;
- Mixing Layers (Fluids);
- Supersonic Jet Flow;
- Acoustic Instability;
- Pressure Distribution;
- Resonance;
- Vortex Sheets;
- Acoustics