Computation of aeroacoustic sources for a Gulfstream G550 nose landing gear model using adaptive FEM
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Publication:1646713
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
computational aeroacousticsFEMadaptive finite element methodscomputational fluid dynamicsTurbulenceCFDCAAlanding gear noise
Hydro- and aero-acoustics (76Q05) Finite element methods applied to problems in fluid mechanics (76M10)
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Uses Software
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
