TY - GEN
T1 - Assessment of Hybrid Delta Wing Vortex Flow Investigation – Part I at Subsonic Conditions
AU - Sedlacek, Dominik
AU - Breitsamter, Christian
AU - Visonneau, Michel
AU - Guilmineau, Emmanuel
AU - Wackers, Jeroen
N1 - Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2022
Y1 - 2022
N2 - The dependencies of numerical simulations regarding grid sensitivity and modelling error for vortex dominated flow need particular investigation. In this study, an extensive investigation on the grid sensitivity is conducted and the influence of different turbulence closures is analyzed. For this purpose, a triple-and a double-delta-wing configuration are considered. In a collaboration between the French National Centre for Scientific Research, the Centrale Nantes Engineering School and the Technical University of Munich, simulations were conducted to identify grid and turbulence closure sensitivities. For the grid sensitivity, a comparison of the global force and moment coefficients and of the local flow in the vortex core is shown. From this, it can be concluded that the local flow is more sensitive to grid adaptation than forces and moments. Furthermore, the double-delta-wing configuration seems to be more affected by grid sensitivity. The comparison of (formula presented) shear stress model, delayed detached eddy simulation and different grids and background closures indicates a lower influence of grid sensitivity to delayed detached eddy simulations than to (formula presented) shear stress models. A grid convergence represents an important parameter but for vortex dominated flows, it can only be achieved by a local convergence for the vortex core flow is of primary importance as vortex core flow characteristics strongly determines the accuracy of the moment prediction.
AB - The dependencies of numerical simulations regarding grid sensitivity and modelling error for vortex dominated flow need particular investigation. In this study, an extensive investigation on the grid sensitivity is conducted and the influence of different turbulence closures is analyzed. For this purpose, a triple-and a double-delta-wing configuration are considered. In a collaboration between the French National Centre for Scientific Research, the Centrale Nantes Engineering School and the Technical University of Munich, simulations were conducted to identify grid and turbulence closure sensitivities. For the grid sensitivity, a comparison of the global force and moment coefficients and of the local flow in the vortex core is shown. From this, it can be concluded that the local flow is more sensitive to grid adaptation than forces and moments. Furthermore, the double-delta-wing configuration seems to be more affected by grid sensitivity. The comparison of (formula presented) shear stress model, delayed detached eddy simulation and different grids and background closures indicates a lower influence of grid sensitivity to delayed detached eddy simulations than to (formula presented) shear stress models. A grid convergence represents an important parameter but for vortex dominated flows, it can only be achieved by a local convergence for the vortex core flow is of primary importance as vortex core flow characteristics strongly determines the accuracy of the moment prediction.
UR - http://www.scopus.com/inward/record.url?scp=85122574613&partnerID=8YFLogxK
U2 - 10.2514/6.2022-0565
DO - 10.2514/6.2022-0565
M3 - Conference contribution
AN - SCOPUS:85122574613
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -