Detached Eddy Simulations of an Airfoil in Turbulent Inflow
Publikation: Forskning - peer review › Konferenceartikel i proceeding
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Detached Eddy Simulations of an Airfoil in Turbulent Inflow. / Gilling, Lasse; Sørensen, Niels; Davidson, Lars.
AIAA Meeting Papers On Disc : 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition: 5 - 8 January 2009, Orlando, Florida. American Institute of Aeronautics & Astronautics, 2009. (Conference Proceeding Series; Nr. 1, Vol. 14).Publikation: Forskning - peer review › Konferenceartikel i proceeding
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RIS
TY - GEN
T1 - Detached Eddy Simulations of an Airfoil in Turbulent Inflow
A1 - Gilling,Lasse
A1 - Sørensen,Niels
A1 - Davidson,Lars
AU - Gilling,Lasse
AU - Sørensen,Niels
AU - Davidson,Lars
PB - American Institute of Aeronautics & Astronautics
PY - 2009
Y1 - 2009
N2 - The effect of resolving inflow turbulence in detached eddy simulations of airfoil flows is studied. Synthetic turbulence is used for inflow boundary condition. The generated turbulence fields are shown to decay according to experimental data as they are convected through the domain with the free stream velocity. The subsonic flow around a NACA 0015 airfoil is studied at Reynolds number 1.6 × 106 and at various angles of attack before and after stall. Simulations with turbulent inflow are compared to experiments and to simulations without turbulent inflow. The results show that the flow is sensitive to the intensity of the resolved turbulence. Especially, when the flow is close to stall, separation can be triggered if the turbulence is resolved. By resolving the inflow turbulence better agreement with experimental data can be achieved.
AB - The effect of resolving inflow turbulence in detached eddy simulations of airfoil flows is studied. Synthetic turbulence is used for inflow boundary condition. The generated turbulence fields are shown to decay according to experimental data as they are convected through the domain with the free stream velocity. The subsonic flow around a NACA 0015 airfoil is studied at Reynolds number 1.6 × 106 and at various angles of attack before and after stall. Simulations with turbulent inflow are compared to experiments and to simulations without turbulent inflow. The results show that the flow is sensitive to the intensity of the resolved turbulence. Especially, when the flow is close to stall, separation can be triggered if the turbulence is resolved. By resolving the inflow turbulence better agreement with experimental data can be achieved.
BT - AIAA Meeting Papers On Disc : 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition
T2 - AIAA Meeting Papers On Disc : 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition
T3 - Conference Proceeding Series
T3 - en_GB
ER -