DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Towards Forced Eddy Simulation of Airframe Induced Noise Radiation from Coherent Hydrodynamic Structures of Jet Flow

Neifeld, Andrej and Ewert, Roland (2018) Towards Forced Eddy Simulation of Airframe Induced Noise Radiation from Coherent Hydrodynamic Structures of Jet Flow. In: 24th AIAA/CEAS Aeroacoustics Conference, 2018 (3463). AIAA. AIAA Aviation Forum 2018, Atlanta, Georgia, USA. doi: 10.2514/6.2018-3463. ISBN 978-162410560-9.

[img] PDF - Only accessible within DLR


The application of Forced Eddy Simulation (FES) is studied in the context of Direct Noise Computation of jet installation noise from nozzle-wing configurations with small relative distance between jet axis and wing trailing edge of the order of the nozzle diameter. Direct noise computations are performed solving the Navier-Stokes equations in perturbation form over a given background RANS flow to realize a zonal RANS/LES simulation approach in the Non-Linear Disturbance Equation (NLDE) framework. The direct noise computation is tackled with a modified version of the full compressible Navier-Stokes equations suitable for moderately compressible flow problems as often present in Computational Aeroacoustics. The formulation enables a formulation of the viscous stress and subfilter contributions in terms of a vector force model that supports an efficient computational treatment. The presented FES method carries on with the development of a stochastic backscatter model for technical applications. The subfilter forcing model provides a combination of dissipation and forcing that yields an additional driving mechanism of the turbulent energy cascade–otherwise not present in purely dissipative models – which enables a rapid onset of fluctuations in the simulation without gray areas. First, simulations of two isolated single stream jets in static condition with nozzle exit Mach number 0.6 and 0.9 are performed to verify the simulation method for the simpler test case of an isolated jet. A second configuration concerns an installed Ultra High Bypass Ratio (UHBR) nozzle below a wing with deployed flap in forward flight at approach condition with a flap deflection of 25°. The simulation considers the entire wind tunnel setup of a related experiment conducted in the Acoustic Windtunnel Braunschweig (AWB).

Item URL in elib:https://elib.dlr.de/122111/
Document Type:Conference or Workshop Item (Speech)
Title:Towards Forced Eddy Simulation of Airframe Induced Noise Radiation from Coherent Hydrodynamic Structures of Jet Flow
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Date:June 2018
Journal or Publication Title:24th AIAA/CEAS Aeroacoustics Conference, 2018
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Forced Eddy Simulation, stochastic backscattering, scale resolving simulation, jet noise, single stream jet, installation effect, jet-flap interaction
Event Title:AIAA Aviation Forum 2018
Event Location:Atlanta, Georgia, USA
Event Type:international Conference
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 (old)
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Technical Acoustics
Deposited By: Neifeld, Dr.-Ing. Andrej
Deposited On:13 Nov 2018 15:50
Last Modified:18 Jul 2023 14:21

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.