journal article·2021-11-01Open access

Study of multi-mode forcing effects on coherent structures of flow transition in a compressible jet

Cong Xu, Huanxin Lai

AIP Advances· Volume 11· Issue 11

Abstract

The disturbances added to trigger turbulence in the simulation of jet flows are mostly implemented with multiple azimuthal modes. The validity and rationale of using such multi-modes are still not very clear. In this paper, large eddy simulations are performed to study a compressible isothermal jet. Flow forcing methods for promoting transition are considered. Two multi-mode disturbances and a single-mode excitation are shown to trigger rapid flow transition, but the development of mixing layers in downstream varies. The most organized vortical structures produced by the vortex rolling/pairing process are observed when the jet is excited by the single-mode forcing, while the shear layers are closer to turbulence when the two multi-mode disturbances are employed. In order to unveil the mechanism behind such differences, dynamic mode decompositions on the axial velocity are conducted to analyze the spatiotemporal coherent structures. The results show that near the nozzle exit, the multi-mode disturbances have triggered more high frequency coherent structures, while the single-mode forcing has produced both low and high frequencies. The low frequency components are transmitted downstream of the jet, leading to poor prediction of the turbulent flow properties.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Aerodynamics and Acoustics in Jet Flows · Fluid Dynamics and Turbulent Flows · Combustion and flame dynamics

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

School of Mechanical and Power Engineering, East China University of Science and Technology , Shanghai 200237, People’s Republic of China

Funding

National Natural Science Foundation of China

References (36)

Show source-provided references
1. Grid sensitivity of flow field and noise of high-Reynolds-number jets computed by large-eddy simulation10.1177/1475472x18778287 ↗
2. Effects of inflow conditions and forcing on subsonic jet flows and noise10.2514/1.7465 ↗
3. Influence of nozzle-exit boundary-layer conditions on the flow and acoustic fields of initially laminar jets10.1017/s0022112010003605 ↗
4. Influence of nozzle-exit boundary-layer profile on high-subsonic jets
5. Influence of initial turbulence level on the flow and sound fields of a subsonic jet at a diameter-based Reynolds number of 10510.1017/jfm.2012.162 ↗
6. Effects of nozzle-exit boundary-layer profile on the initial shear-layer instability, flow field and noise of subsonic jets10.1017/jfm.2019.546 ↗
7. Importance of the nozzle-exit boundary-layer state in subsonic turbulent jets10.1017/jfm.2018.476 ↗
8. Roles of initial condition and vortex pairing in jet noise10.1016/0022-460x(87)90540-2 ↗
9. Laminar and turbulent nozzle-jet flows and their acoustic near-field10.1063/1.4890493 ↗
10. Index of resolution quality for large eddy simulations10.1115/1.1990201 ↗
11. Numerical analysis of the impact of exit conditions on low Mach number turbulent jets10.1016/j.ijheatfluidflow.2017.07.003 ↗
12. A large-eddy simulation of a high Reynolds number Mach 0.9 jet
13. Transition to turbulence and noise radiation in heated coaxial jet flows10.1063/1.4944753 ↗
14. Jet noise measurements: Past and present10.1260/1475-472x.9.4-5.559 ↗
15. Effects of the initial boundary-layer state on turbulent jet mixing10.2514/3.61491 ↗
16. Large eddy simulation of plane jet sound radiation
17. Axisymmetric mixing layer: Influence of the initial and boundary conditions10.2514/3.61061 ↗
18. Coherent structures and turbulence10.1017/s0022112086001192 ↗
19. Final results from single point measurements
20. Results from acoustic field measurements
21. Numerical study of eigenmode forcing effects on jet flow development and noise generation mechanisms10.1063/1.3112686 ↗
22. Analysis of noise radiation mechanisms in hot subsonic jet from a validated large eddy simulation solution10.1063/1.4926792 ↗
23. On the hydrodynamic and acoustic nature of pressure proper orthogonal decomposition modes in the near field of a compressible jet10.1017/jfm.2017.839 ↗
24. Survey on jet instability theory10.1016/0376-0421(84)90005-8 ↗
25. Effect of the Reynolds number on the aeroacoustic fields of a transitional supersonic jet10.1063/1.5138195 ↗
26. Dynamic mode decomposition of numerical and experimental data10.1017/s0022112010001217 ↗
27. Decomposition of time-resolved tomographic PIV10.1007/s00348-012-1266-8 ↗
28. An experimental study of jet noise Part I: Turbulent mixing noise10.1016/0022-460x(77)90493-x ↗
29. Aeroacoustics of hot jets10.1017/s0022112004000151 ↗
30. Large eddy simulation of jet noise from unstructured grids with turbulent nozzle boundary layer
31. Large eddy simulation of hot jets and evaluation of grid resolution
32. Effects of flow forcing on simulation of subsonic turbulent jet flow and noise10.14135/j.cnki.1006-3080.20200603001 ↗
33. Large-scale structure in the mixing layer of a round jet10.1017/s0022112078002670 ↗
34. Effect of initial boundary-layer state on subsonic jet noise10.2514/1.j051712 ↗
35. Increased jet noise due to a ‘nominally laminar’ state of nozzle exit boundary layer
36. Isothermal and heated subsonic jet noise using large eddy simulations on unstructured grids10.1016/j.compfluid.2018.06.003 ↗