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Numerical Simulation of Aerodynamic Noise with DLR's aeroacoustic code PIANO

Delfs, Jan W. and Bauer, Marcus and Ewert, Roland and Grogger, Herwig A. and Lummer, Markus and Lauke, Thomas G.W. (2008) Numerical Simulation of Aerodynamic Noise with DLR's aeroacoustic code PIANO. DLR - Elib. [Other]

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The code PIANO, developed at the Institute of Aerodynamics and Flow Technology (Dept. Technical Acoustics), is designed to simulate aeroacoustic noise generation and acoustic wave propagation in non-uniform flows. It is based on the equations governing the inviscid dynamics of perturbations to a given time-averaged mean flow field. PIANO simulates the noise generation process, when vorticity interacts with solid structures or gradients in the flow field. PIANO is not designed to calculate wave propagation over very large distances in uniform flows, like from aircraft to ground. In that case methods based on wave equations are more appropriate. Currently, PIANO is based on structured, curvilinear multi-block grids. The coding structure is designed for high performance on workstations, vector machines, PCs or PC clusters as well. PIANO is a research code.

Item URL in elib:https://elib.dlr.de/118928/
Document Type:Other
Title:Numerical Simulation of Aerodynamic Noise with DLR's aeroacoustic code PIANO
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Delfs, Jan W.jan.delfs (at) dlr.deUNSPECIFIED
Bauer, Marcusmarcus.bauer (at) dlr.deUNSPECIFIED
Ewert, Rolandroland.ewert (at) dlr.deUNSPECIFIED
Grogger, Herwig A.herwig.grogger (at) dlr.deUNSPECIFIED
Lummer, Markusmarkus.lummer (at) dlr.deUNSPECIFIED
Lauke, Thomas G.W.thomas.lauke (at) dlr.deUNSPECIFIED
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
Number of Pages:116
Publisher:DLR - Elib
Keywords:Computational Aeroacoustics, CAA, Aeroacoustics, Aeroakustik, Linearized Euler Equations, LEE, Acoustic Perturbation Equations, APE
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Technical Acoustics
Deposited By: Delfs, Prof.Dr. Jan Werner
Deposited On:12 Feb 2018 14:42
Last Modified:31 Jul 2019 20:16

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