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Numerical research of dynamic derivatives of unsteady moved aircraft

Hübner, Andreas-Rene (2008) Numerical research of dynamic derivatives of unsteady moved aircraft. In: VKI Lecture Series, Experimental Determination of Dynamic Stability Parameters VKI Lecture Series, 2008-02. ISBN 978-2-930389-81-8.

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Abstract

The investigations presented in this lecture notes are concerned with simulation of unsteady aircraft aerodynamics and thus belong to the research field of computational fluid dynamics (CFD) for aerospace applications. For the determination of static and dynamic derivatives the calculations are based on the panel method VSAERO and on the solution of the Reynolds-averaged Navier-Stokes (RANS) equations using the finite volume parallel solution algorithm with an unstructured discretization concept (DLR TAU-code). Systematic investigations have been performed with simple configurations based on NACA0012 airfoil sections (e.g. wing, wing with horizontal tail, wing with vertical tail) in order to obtain a more detailed understanding of the unsteady aerodynamical and flight mechanical behavior of such configurations. Further calculations were performed for a set of experimental data measured on a generic modern transport aircraft configuration (DLR-F12) tested in the 3m Low Speed Wind Tunnel NWB of the German-Dutch Wind Tunnels DNW, Germany, using a unique six degree-of-freedom test rig called 'Model Positioning Mechanism' (MPM). One objective of this investigation is to adapt the numerical methods for the calculations of dynamic derivatives and to validate the numerical methods by means of wind tunnel data.

Item URL in elib:https://elib.dlr.de/53562/
Document Type:Contribution to a Collection
Title:Numerical research of dynamic derivatives of unsteady moved aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hübner, Andreas-ReneUNSPECIFIEDUNSPECIFIED
Date:18 February 2008
Journal or Publication Title:VKI Lecture Series, Experimental Determination of Dynamic Stability Parameters
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:2008-02
Editors:
EditorsEmail
VKI, UNSPECIFIED
Series Name:VKI Lecture Series
ISBN:978-2-930389-81-8
Status:Published
Keywords:unsteady aerodynamic, dynamic derivative, DLR-F12 geometry, quasi-steady motion, unsteady motion, numerical simulation
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Configuration Design
Deposited By: Hübner, Andreas-Rene
Deposited On:03 Mar 2009
Last Modified:27 Apr 2009 14:48

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