Back to Search
Start Over
Verification and application of a mean flow perturbation method for jet noise
- Source :
- IndraStra Global.
- Publication Year :
- 2018
- Publisher :
- ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER, 2018.
-
Abstract
- The stability properties of basic states are often elucidated by examining the evolution of small disturbances. Such studies have recently been successfully applied to mean turbulent states, obtained through averaging of experimental measurements or Large-Eddy Simulations (LES), for both wall-bounded as well as free shear flows. Typically, the equations are employed using the disturbance form of the equations. To circumvent the necessity to linearize the governing equations, an especially tedious task for viscous and turbulent closure terms, Touber and Sandham (2009) [21], proposed an approach that achieves the same purpose by solving the full Navier-Stokes (NS) equations, with a forcing term to maintain mean flow invariance. The method places no restrictions, such as slow streamwise variations, on the underlying basic state. The goals of the current work are to first verify this mean flow perturbation (NS-MFP) technique and then apply it to the problem of jet noise. For the first thrust, we show that when the basic state is appropriately constrained, the technique reverts to Linear, Parabolized and Global stability methods. The method is then verified by reproducing the growth of unstable modes in an inviscid Mach 6 entropy layer. The application to jet noise considers subsonic Mach 0.9 and perfectly expanded supersonic Mach 1.3 round jets. The results are compared with those from Parabolized Stability Equations (PSE) and LES solutions, respectively, considering monochromatic and multi-frequency perturbations. The NS-MFP method successfully reproduces key features of the modal response, including Strouhal number dependent directivity of noise radiation. Aspects related to the manner in which the mean basic state is obtained, whether from LES or Reynolds-averaged Navier-Stokes (RANS) equation are also explored. In particular, the sensitivity of the perturbation to whether the eddy viscosity is included or not, is examined in reference to maximum intensity of pressure fluctuation, directivity of noise radiation and the rate of fall-off of the spectra at higher Strouhal numbers. The results indicate that a closer match on the noise-radiation characteristics is obtained when effects of eddy-viscosity on the disturbances are neglected. (C) 2018 Elsevier Masson SAS. All rights reserved.
- Subjects :
- MODELS
Global stability analysis
PARABOLIZED STABILITY EQUATIONS
Aerospace Engineering
01 natural sciences
Jet noise
010305 fluids & plasmas
Navier-Stokes equation
Physics::Fluid Dynamics
symbols.namesake
Parabolized stability equation (PSE)
Inviscid flow
0103 physical sciences
Mean flow
010306 general physics
WAVE/BOUNDARY-LAYER INTERACTIONS
Physics
LARGE-EDDY SIMULATION
UNSTEADINESS
Turbulence
Linear stability theory (LST)
Turbulence modeling
Stability analysis
Large-eddy simulations
BOUNDARY-LAYER
Mechanics
COLD JET
GLOBAL LINEAR INSTABILITY
Mach number
SHEAR LAYERS
symbols
Strouhal number
WAVE
Reynolds-averaged Navier–Stokes equations
Subjects
Details
- Language :
- English
- ISSN :
- 23813652
- Database :
- OpenAIRE
- Journal :
- IndraStra Global
- Accession number :
- edsair.doi.dedup.....33e2af53f4330a96cc86c3bde3393784