Adjoint Linearised Euler solver and Source Modelling for Goldstein acoustic analogy equations for 3D jet flow problems: verification and capability study
نویسندگان
چکیده
The Adjoint Linearised Euler Solver of Karabasov and Hynes (2006), which includes an efficient iterative solution of linearised Euler equations in the frequency domain, has been extended to a 3D framework. Numerical tests performed for the problem of sound scattering from an axi-symmetric Gaussian jet flow show a very good performance of the method for a range of frequencies and observer angles as compared with the reference semianalytical solution. A new approach has been introduced for evaluating the source terms of the Goldstein acoustic analogy equations based on the second-order statistics provided directly from Large Eddy Simulation (LES). In comparison with the previous works, the new procedure is completely free from modelling assumptions, such as the functional behavior of the auto-covariance stress tensor or the dependence of the correlation scales of frequency. This makes the Goldstein acoustic analogy modelling based on LES practically applicable to general 3D flows and allows not only computing the far-field pressure spectra but also the reconstruction of effective volume noise sources. In comparison with the standard integral surface methods such as the Ffowcs Williams – Hawkings (FW-H) penetrable surface formulation, the new approach is potentially more robust since it has no sensitivity to the acoustic surface location. For the proof-of-concept study, acoustic predictions are made for two static single-stream co-axial jets at acoustic Mach number V /c = 0.875 that correspond to the temperature ratios T /T = 1 and T /T = 2.5. Comparisons with the reference penetrable FW-H solutions and the scaled QinetiQ experiment data are performed. The budgets of acoustic power spectral density for the individual source terms of the acoustic analogy model are also provided.
منابع مشابه
A New Implicit Dissipation Term for Solving 3D Euler Equations on Unstructured Grids by GMRES+LU-SGS Scheme
Due to improvements in computational resources, interest has recently increased in using implicit scheme for solving flow equations on 3D unstructured grids. However, most of the implicit schemes produce greater numerical diffusion error than their corresponding explicit schemes. This stems from the fact that in linearizing implicit fluxes, it is conventional to replace the Jacobian matrix in t...
متن کاملA New Implicit Dissipation Term for Solving 3D Euler Equations on Unstructured Grids by GMRES+LU-SGS Scheme
Due to improvements in computational resources, interest has recently increased in using implicit scheme for solving flow equations on 3D unstructured grids. However, most of the implicit schemes produce greater numerical diffusion error than their corresponding explicit schemes. This stems from the fact that in linearizing implicit fluxes, it is conventional to replace the Jacobian matrix in t...
متن کاملA High-Order Finite Element Method for the Linearised Euler Equations
Sound propagation in complex non-uniform mean flows is an important feature of turbofan exhaust noise radiation. The Linearised Euler Equations are able to represent the strong shear layer refraction effects on the sound field, as well as multiple length scales. Frequency domain solvers are suitable for tonal noise and considered a way to avoid linear instabilities, which may occur with time do...
متن کاملComputation of Mode Radiation from a Generic Aeroengine Intake
The radiation of acoustic modes from an aeroengine intake duct is reviewed. The method is based upon a computational scheme which allows acoustic waves, propagating inside the intake duct of a generic aircraft engine, to be admitted into a computational domain that includes the duct section, the exit plane of the duct, and the surrounding flow. The method comprises three elements: a matching pr...
متن کاملAdaptation of Structured Grid for Supersonic and Transonic Flows
Two distinct redistribution grids - adaptation techniques, spring analogy and elliptic grid generator are applied to two-dimensional steady, inviscid, shocked flows, and the ability of each technique is examined and compared. Euler equations are solved base on Roe's Reimann solver approach to simulate supersonic flow around a sphere, transonic flow about an airfoil and supersonic flow in a symm...
متن کامل