Computation of aeroacoustic sources for a Gulfstream G550 nose landing gear model using adaptive FEM

DOI10.1016/j.compfluid.2015.10.017zbMath1390.76831OpenAlexW1919461791WikidataQ125764779 ScholiaQ125764779MaRDI QIDQ1646713

Niclas Jansson, Johan Hoffman, Rodrigo Vilela De Abreu

Publication date: 26 June 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2015.10.017

zbMATH Keywords

computational aeroacousticsFEMadaptive finite element methodscomputational fluid dynamicsTurbulenceCFDCAAlanding gear noise

Mathematics Subject Classification ID

Hydro- and aero-acoustics (76Q05) Finite element methods applied to problems in fluid mechanics (76M10)

Related Items

New theory of flight ⋮ A high-order residual-based viscosity finite element method for incompressible variable density flow ⋮ Adaptive modeling of turbulent flow with residual based turbulent kinetic energy dissipation ⋮ Towards a parameter-free method for high Reynolds number turbulent flow simulation based on adaptive finite element approximation

Uses Software

• FEniCS
• Unicorn
• FUN3D

Cites Work

• Subgrid scale model for finite difference simulations of turbulent flows in plane channels and annuli
• A new approach to computational turbulence modeling
• Computational Turbulent Incompressible Flow
• Adaptive simulation of the subcritical flow past a sphere
• Efficient computation of mean drag for the subcritical flow past a circular cylinder using general Galerkin G2
• Adaptive computation of aeroacoustic sources for a rudimentary landing gear
• Computation of Mean Drag for Bluff Body Problems Using Adaptive DNS/LES
• On sound generated aerodynamically I. General theory