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Coupled CFD-CAA Simulations for the Airbus A400M Propeller 15.01 Validation Case

Stuermer, Arne and Yin , Jianping (2009) Coupled CFD-CAA Simulations for the Airbus A400M Propeller 15.01 Validation Case. DLR-Interner Bericht. IB 124-2009/908, 34 S.

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Abstract

Under contract to Airbus France the DLR Institute of Aerodynamics and Flow Technology performed a coupled CFD (Computational Fluid Dynamics) and CAA (Computational Aeroacoustics) simulation of the A400M-Propeller at cruise flight conditions. The configuration under study, termed the A400M 15.01 cruise validation case by Airbus, is the isolated inboard propeller of the Airbus A400M military transport aircraft, which includes the nacelle with a chin-mounted inlet. The fully unsteady aerodynamic simulations were performed with the DLR TAU-Code. The results of these simulations serve as input data to the aeroacoustic analysis, which was done with the DLR APSIM-Code. The aim of the study was to determine the suitability of the numerical methods to the aerodynamic and aeroacoustic simulations of the complex flow physics of propeller propulsion systems. This report describes the approach applied by DLR to the simulation and presents the results. The validation of the numerical predictions is not covered in this report, as this was done in house at the contractor.

Document Type:Monograph (DLR-Interner Bericht)
Title:Coupled CFD-CAA Simulations for the Airbus A400M Propeller 15.01 Validation Case
Authors:
AuthorsInstitution or Email of Authors
Stuermer, Arnearne.stuermer@dlr.de
Yin , Jianpingjianping.yin@dlr.de
Date:September 2009
Number of Pages:34
Keywords:CFD uRANS TAU, Propeller, High Speed, Propeller Loads and Performance, Aeroacoustic APSIM, quadrupole (nonlinear) noise
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Quiet and Comfortable Rotorcraft
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Dr.-Ing. Jianping Yin
Deposited On:28 Sep 2011 16:12
Last Modified:28 Sep 2011 16:12

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