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Influence of Vertical Stabilizer on the Aerodynamic Stability of a Generic Multi Delta Wing Aircraft Configuration

Alt, Katharina and Schütte, Andreas (2023) Influence of Vertical Stabilizer on the Aerodynamic Stability of a Generic Multi Delta Wing Aircraft Configuration. In: 23rd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIV, 14, pp. 637-646. Springer Nature. 22. DGLR-Fachsymposium der STAB, 2022-11-09 - 2022-11-10, Berlin, Deutschland. doi: 10.1007/978-3-031-40482-5_60. ISBN 978-3-031-40481-8. ISSN 1612-2909.

Full text not available from this repository.

Official URL: https://link.springer.com/chapter/10.1007/978-3-031-40482-5_60

Abstract

The current numerical investigations analyze the influence of the vertical stabilizer on the aerodynamics and aerodynamic stability, especially roll stability, of a multi delta wing configuration. Planform studies established to enhance the rolling moment behavior by means of strakes and wing leading edge slats are taken as a reference for the current vertical tail plane studies. The aim is to identify the differences between the configuration with and without vertical tails. In particular the influence of the vortical flow topology and interaction with the vertical tail planes on the aerodynamic behavior should be identified. This should lead to design recommendations for the current fighter design approaches within the DLR project Diabolo

Item URL in elib:https://elib.dlr.de/203225/
Document Type:Conference or Workshop Item (Speech)
Title:Influence of Vertical Stabilizer on the Aerodynamic Stability of a Generic Multi Delta Wing Aircraft Configuration
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Alt, KatharinaKatharina.Alt (at) dlr.deUNSPECIFIEDUNSPECIFIED
Schütte, AndreasAndreas.Schuette (at) dlr.deUNSPECIFIEDUNSPECIFIED
Date:23 September 2023
Journal or Publication Title:23rd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIV
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:14
DOI:10.1007/978-3-031-40482-5_60
Page Range:pp. 637-646
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Dillmann, AndreasAndreas.Dillmann (at) dlr.deUNSPECIFIEDUNSPECIFIED
Heller, Gerdgerd.heller (at) airbus.comUNSPECIFIEDUNSPECIFIED
Krämer, EwaldInstitut für Aerodynamik und Gasdynamik Universität StuttgartUNSPECIFIEDUNSPECIFIED
Wagner, ClausClaus.Wagner (at) dlr.dehttps://orcid.org/0000-0003-2273-0568UNSPECIFIED
Weiss, JulienUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Publisher:Springer Nature
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-031-40481-8
Status:Published
Keywords:computational fluid dynamics, vortex flow, vertical stabilizer, delta wing aerodynamics, aerodynamic stability
Event Title:22. DGLR-Fachsymposium der STAB
Event Location:Berlin, Deutschland
Event Type:national Conference
Event Start Date:9 November 2022
Event End Date:10 November 2022
Organizer:TU Berlin
HGF - Research field:other
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L DT - Defense Technology
DLR - Research theme (Project):L - Effect
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology
Deposited By: Schütte, Andreas
Deposited On:28 Jul 2025 13:39
Last Modified:26 Aug 2025 10:19

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