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Static and dynamic numerical simulations of a generic UCAV configuration with and without control devices

Schütte, Andreas and Huber, Kerstin Claudie and Boelens, Okko J. (2014) Static and dynamic numerical simulations of a generic UCAV configuration with and without control devices. In: 32nd AIAA Applied Aerodynamics Conference (2132), pp. 1-26. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, USA.

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Official URL: http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2132

Abstract

A contribution for the assessment of the static and dynamic aerodynamic behavior of a generic UCAV configuration with control devices using CFD methods is given. For the CFD simulations the unstructured grid based DLR TAU-Code and the structured grid based NLR solver ENSOLV are used. The numerical methods are verified by experimental wind tunnel data. The current investigations should provide a contribution to assess the prediction capability of control device effectiveness using CFD methods. The presented computational results for the assessment will be validated by dedicated experimental data. Furthermore, it should support the understanding of the flow physics around the trailing edge control devices of highly swept configurations with a vortex dominated flow field. Design requirements should be able draw by analyzing the interaction between the vortical flow and the control devices. The present work is part of the NATO STO/AVT Task Group AVT-201 on Stability and Control prediction methods

Item URL in elib:https://elib.dlr.de/90254/
Document Type:Conference or Workshop Item (Speech)
Additional Information:DOI: 10.2514/6.2014-2132
Title:Static and dynamic numerical simulations of a generic UCAV configuration with and without control devices
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schütte, Andreasandreas.schuette (at) dlr.deUNSPECIFIED
Huber, Kerstin Claudiekerstin.huber (at) dlr.deUNSPECIFIED
Boelens, Okko J.Okko.Boelens (at) nlr.nlUNSPECIFIED
Date:June 2014
Journal or Publication Title:32nd AIAA Applied Aerodynamics Conference
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-26
Status:Published
Keywords:UCAV, vortical flow, CFD, DLR-TAU, ENSOLV, Validiation, Stability and Control
Event Title:32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA
Event Location:USA
Event Type:international Conference
Event Dates:16.-20. Juni 2014
Organizer:AIAA
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 - Military Technologies
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Schütte, Andreas
Deposited On:03 Sep 2014 15:19
Last Modified:31 Jul 2019 19:47

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