@inbook{c46a23c4c2724718baf8e625d50fc423,
title = "Analysis of Vortex Burst Phenomena on Generic Hybrid Delta Wing Planforms at Subsonic Speeds",
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.",
keywords = "Fast Response Aerodynamic probe, Hybrid delta wings, Vortex breakdown",
author = "Dominik Sedlacek and Heckmeier, \{Florian M.\} and Artur Usbek and Christian Breitsamter",
note = "Publisher Copyright: {\textcopyright} 2021, The Author(s), under exclusive license to Springer Nature Switzerland AG.",
year = "2021",
doi = "10.1007/978-3-030-79561-0\_27",
language = "English",
series = "Notes on Numerical Fluid Mechanics and Multidisciplinary Design",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "282--291",
booktitle = "Notes on Numerical Fluid Mechanics and Multidisciplinary Design",
}