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Document type:
Buchbeitrag 
Author(s):
Sedlacek, Dominik; Heckmeier, Florian M.; Usbek, Artur; Breitsamter, Christian 
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...    »
 
Keywords:
Fast Response Aerodynamic probe; Hybrid delta wings; Vortex breakdown 
Dewey Decimal Classification:
620 Ingenieurwissenschaften 
Book title:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design 
Publisher:
Springer International Publishing 
Date of publication:
14.07.2021 
Year:
2021 
Pages:
282-291 
Covered by:
Scopus 
Print-ISBN:
978-3-030-79560-3 
E-ISBN:
978-3-030-79561-0 
Language:
en 
Notes:
Funding text 1 The project is funded by the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) ? grant number BR1511/13-1. The fruitful cooperation with Airbus Defense and Space is gratefully acknowledged. Funding text 2 Acknowledgments. The project is funded by the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) – grant number BR1511/13-1. The fruitful cooperation with Airbus Defense and Space is gratefully acknowledged. 
TUM Institution:
Lehrstuhl für Aerodynamik und Strömungsmechanik