Detached Eddy Simulations of an Airfoil in Turbulent Inflow

Publication: Research - peer-review › Article in proceeding

Standard

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; No. 1, Vol. 14).

Publication: Research - peer-review › Article in proceeding

Harvard

Gilling, L , Sørensen, N & Davidson, L 2009, 'Detached Eddy Simulations of an Airfoil in Turbulent Inflow'. in 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. Conference Proceeding Series, no. 1, vol. 14

APA

Gilling, L., Sørensen, N., & Davidson, L. (2009). Detached Eddy Simulations of an Airfoil in Turbulent Inflow. In AIAA Meeting Papers On Disc : 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics & Astronautics. (Conference Proceeding Series; No. 1, Vol. 14).

CBE

Gilling L , Sørensen N, Davidson L. 2009. Detached Eddy Simulations of an Airfoil in Turbulent Inflow. In 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. (Conference Proceeding Series; No. 1, Vol. 14).

MLA

Gilling, Lasse , NielsSørensen and LarsDavidson "Detached Eddy Simulations of an Airfoil in Turbulent Inflow". 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; ???journalNumber??? 1, ???volume??? 14).

Vancouver

Gilling L , Sørensen N, Davidson L. Detached Eddy Simulations of an Airfoil in Turbulent Inflow. In 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; No. 1, Vol. 14).

Author

Gilling, Lasse ; Sørensen, Niels; Davidson, Lars / Detached Eddy Simulations of an Airfoil in Turbulent Inflow.

Publication: Research - peer-review › Article in proceeding

Bibtex

@inbook{409ca0e07aa611de9240000ea68e967b,

title = "Detached Eddy Simulations of an Airfoil in Turbulent Inflow",

publisher = "American Institute of Aeronautics & Astronautics",

author = "Lasse Gilling and Niels Sørensen and Lars Davidson",

year = "2009",

series = "Conference Proceeding Series",

booktitle = "AIAA Meeting Papers On Disc : 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition",

}

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 -