Analysis of Vortex Burst Phenomena on Generic Hybrid Delta Wing Planforms at Subsonic Speeds

Dominik Sedlacek, Florian M. Heckmeier, Artur Usbek, Christian Breitsamter

Publikation: Beitrag in Buch/Bericht/KonferenzbandKapitelBegutachtung

3 Zitate (Scopus)

Abstract

In this study, experimental investigations are performed to analyze the vortex behavior and breakdown characteristics on a generic multiple swept wing fuselage configuration. Fast Response Aerodynamic Pressure Probe and Particle Image Velocimetry measurements are performed in the low-speed wind tunnel W/T-A facility of the Chair of Aerodynamics and Fluid Mechanics at the Technical University of Munich. The experiments are executed at subsonic speed, symmetric freestream conditions and angles of attack of α= 16 , 24 and 32 . In a power spectral density analysis of velocity fluctuations helical mode instabilities and shear layer instabilities can be detected.

OriginalspracheEnglisch
TitelNotes on Numerical Fluid Mechanics and Multidisciplinary Design
Herausgeber (Verlag)Springer Science and Business Media Deutschland GmbH
Seiten282-291
Seitenumfang10
DOIs
PublikationsstatusVeröffentlicht - 2021

Publikationsreihe

NameNotes on Numerical Fluid Mechanics and Multidisciplinary Design
Band151
ISSN (Print)1612-2909
ISSN (elektronisch)1860-0824

Fingerprint

Untersuchen Sie die Forschungsthemen von „Analysis of Vortex Burst Phenomena on Generic Hybrid Delta Wing Planforms at Subsonic Speeds“. Zusammen bilden sie einen einzigartigen Fingerprint.

Dieses zitieren