Computational aeroacoustics: progress on nonlinear problems of sound generation

T Colonius, SK Lele - Progress in Aerospace sciences, 2004 - Elsevier
Computational approaches are being developed to study a range of problems in
aeroacoustics. These aeroacoustic problems may be classified based on the physical …

Combustion and engine-core noise

M Ihme - Annual Review of Fluid Mechanics, 2017 - annualreviews.org
The implementation of advanced low-emission aircraft engine technologies and the
reduction of noise from airframe, fan, and jet exhaust have made noise contributions from an …

[HTML][HTML] Combustion noise

AP Dowling, Y Mahmoudi - Proceedings of the Combustion Institute, 2015 - Elsevier
Combustion noise is becoming increasingly important as a major noise source in
aeroengines and ground based gas turbines. This is partially because advances in design …

[图书][B] Numerical simulation of mechatronic sensors and actuators

M Kaltenbacher - 2007 - Springer
Each modern industrial process environment needs sensors to detect the physical quantities
involved (eg, electric current, mechanical torque, temperature, etc.), a signal-conditioning …

[HTML][HTML] Nektar++: Enhancing the capability and application of high-fidelity spectral/hp element methods

D Moxey, CD Cantwell, Y Bao, A Cassinelli… - Computer Physics …, 2020 - Elsevier
Nektar++ is an open-source framework that provides a flexible, high-performance and
scalable platform for the development of solvers for partial differential equations using the …

Hybrid aeroacoustic computations: State of art and new achievements

S Schoder, M Kaltenbacher - Journal of Theoretical and …, 2019 - World Scientific
This paper collects the state of the art and the tremendous progress that has been made in
hybrid modeling of aeroacoustic sound. Hybrid modeling is defined such that flow and …

Broadband slat noise prediction based on CAA and stochastic sound sources from a fast random particle-mesh (RPM) method

R Ewert - Computers & Fluids, 2008 - Elsevier
The application of a low-cost computational aeroacoustics (CAA) approach to a slat noise
problem is studied. A fast and efficient stochastic method is introduced to model the …

Adaptive numerical simulations with Trixi. jl: A case study of Julia for scientific computing

H Ranocha, M Schlottke-Lakemper, AR Winters… - arXiv preprint arXiv …, 2021 - arxiv.org
We present Trixi. jl, a Julia package for adaptive high-order numerical simulations of
hyperbolic partial differential equations. Utilizing Julia's strengths, Trixi. jl is extensible, easy …

[HTML][HTML] Computational aeroacoustics of the EAA benchmark case of an axial fan

S Schoder, C Junger… - Acta Acustica, 2020 - acta-acustica.edpsciences.org
This contribution benchmarks the aeroacoustic workflow of the perturbed convective wave
equation and the Ffowcs Williams and Hawkings analogy in Farassat's 1A version for a low …

Linearized perturbed compressible equations for low Mach number aeroacoustics

JH Seo, YJ Moon - Journal of Computational Physics, 2006 - Elsevier
For efficient aeroacoustic computation at low Mach numbers, the linearized perturbed
compressible equations (LPCE) are proposed. The derivation is based on investigation of …