Hydrodynamic/acoustic splitting approach with flow-acoustic feedback for universal subsonic noise computation
نویسندگان
چکیده
A generalized approach to decompose the compressible Navier-Stokes equations into an equivalent set of coupled for flow and acoustics is introduced. As a significant extension standard hydrodynamic/acoustic splitting methods, provides essential coupling terms, which account feedback from flow. unique simplified version split equation system with derived that conforms in subsonic regime, where reduces one additional term momentum equation. Subsonic simulations are conducted flow-acoustic cases using scale-resolving run-time hierarchical Cartesian mesh solver, operates different explicit time step sizes incompressible acoustics. The first simulation case focuses on tone generic flute. With major included, yields characteristics agreement reference results K\"uhnelt based Lattice-Boltzmann simulation. On contrary, hybrid method feedback-term switched off lacks proper tone. second case, thick plate duct studied at various low Mach numbers around Parker-beta-mode resonance. reveal mechanism very good experimental data Welsh et al. Simulations theoretical considerations does not reduce stable convective size equations.
منابع مشابه
Aerodynamic Noise Computation of the Flow Field around NACA 0012 Airfoil Using Large Eddy Simulation and Acoustic Analogy
The current study presents the results of the aerodynamic noise prediction of the flow field around a NACA 0012 airfoil at a chord-based Reynolds number of 100,000 and at 8.4 degree angle of attack. An incompressible Large Eddy Simulation (LES) turbulence model is applied to obtain the instantaneous turbulent flow field. The noise prediction is performed by the Ffowcs Williams and Hawkings (FW-...
متن کاملaerodynamic noise computation of the flow field around naca 0012 airfoil using large eddy simulation and acoustic analogy
the current study presents the results of the aerodynamic noise prediction of the flow field around a naca 0012 airfoil at a chord-based reynolds number of 100,000 and at 8.4 degree angle of attack. an incompressible large eddy simulation (les) turbulence model is applied to obtain the instantaneous turbulent flow field. the noise prediction is performed by the ffowcs williams and hawkings (fw-...
متن کاملComputation of the Flow of a Dual-Stream Jet with Fan-Flow Deflectors for Noise Reduction
This paper studies the impact of installing noise-suppressing deflector vanes in the bypass flow on the aerodynamic performance of the dual-stream supersonic nozzle of a turbofan engine by using a three-dimensional Reynolds-averaged Navier-Stokes computer program. A series of nozzle configurations using a single pair or double pairs of vanes with NACA0012, NACA4412, and NACA7514 airfoil profile...
متن کاملUniversal photonic quantum computation via time-delayed feedback.
We propose and analyze a deterministic protocol to generate two-dimensional photonic cluster states using a single quantum emitter via time-delayed quantum feedback. As a physical implementation, we consider a single atom or atom-like system coupled to a 1D waveguide with a distant mirror, where guided photons represent the qubits, while the mirror allows the implementation of feedback. We iden...
متن کاملNonlinear interaction model of subsonic jet noise.
Noise generation in a subsonic round jet is studied by a simplified model, in which nonlinear interactions of spatially evolving instability modes lead to the radiation of sound. The spatial mode evolution is computed using linear parabolized stability equations. Nonlinear interactions are found on a mode-by-mode basis and the sound radiation characteristics are determined by solution of the Li...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: Journal of Computational Physics
سال: 2021
ISSN: ['1090-2716', '0021-9991']
DOI: https://doi.org/10.1016/j.jcp.2021.110548