TY - JOUR
T1 - Large eddy simulation of a sheet/cloud cavitation on a NACA0015 hydrofoil
AU - Wang, G.
AU - Ostoja-Starzewski, M.
N1 - Funding Information:
We thank an anonymous reviewer for all the comments. Work of the first author was supported by the US Navy. The second author acknowledges the support by the Canada Research Chairs program.
PY - 2007/3
Y1 - 2007/3
N2 - A single fluid model of sheet/cloud cavitation is developed and applied to a NACA0015 hydrofoil. First, a cavity formation model is set up, based on a three-dimensional (3D) non-cavitation model of Navier-Stokes equations with a large eddy simulation (LES) scheme for weakly compressible flows. A fifth-order polynomial curve is adopted to describe the relationship between density coefficient ratio and pressure coefficient when cavitation occurs. The Navier-Stokes equations including cavitation bubble clusters are solved using the finite-volume approach with time-marching scheme, and MacCormack's explicit-corrector scheme is adopted. Simulations are carried out in a 3D field acting on a hydrofoil NACA0015 at angles of attack 4°, 8° and 20°, with cavitation numbers σ = 1.0, 1.5 and 2.0, Re = 106, and a 360 × 63 × 29 meshing system. We study time-dependent sheet/cloud cavitation structures, caused by the interaction of viscous objects, such as vortices, and cavitation bubbles. At small angles of attack (4°), the sheet cavity is relatively stable just by oscillating in size at the accumulation stage; at 8° it has a tendency to break away from the upper foil section, with the cloud cavitation structure becoming apparent; at 20°, the flow separates fully from the leading edge of the hydrofoil, and the vortex cavitation occurs. Comparisons with other studies, carried out mainly in the context of flow patterns on which prior experiments and simulations were done, demonstrate the power of our model. Overall, it can snapshot the collapse of cloud cavitation, and allow a study of flow patterns and their instabilities, such as "crescent-shaped regions.".
AB - A single fluid model of sheet/cloud cavitation is developed and applied to a NACA0015 hydrofoil. First, a cavity formation model is set up, based on a three-dimensional (3D) non-cavitation model of Navier-Stokes equations with a large eddy simulation (LES) scheme for weakly compressible flows. A fifth-order polynomial curve is adopted to describe the relationship between density coefficient ratio and pressure coefficient when cavitation occurs. The Navier-Stokes equations including cavitation bubble clusters are solved using the finite-volume approach with time-marching scheme, and MacCormack's explicit-corrector scheme is adopted. Simulations are carried out in a 3D field acting on a hydrofoil NACA0015 at angles of attack 4°, 8° and 20°, with cavitation numbers σ = 1.0, 1.5 and 2.0, Re = 106, and a 360 × 63 × 29 meshing system. We study time-dependent sheet/cloud cavitation structures, caused by the interaction of viscous objects, such as vortices, and cavitation bubbles. At small angles of attack (4°), the sheet cavity is relatively stable just by oscillating in size at the accumulation stage; at 8° it has a tendency to break away from the upper foil section, with the cloud cavitation structure becoming apparent; at 20°, the flow separates fully from the leading edge of the hydrofoil, and the vortex cavitation occurs. Comparisons with other studies, carried out mainly in the context of flow patterns on which prior experiments and simulations were done, demonstrate the power of our model. Overall, it can snapshot the collapse of cloud cavitation, and allow a study of flow patterns and their instabilities, such as "crescent-shaped regions.".
KW - Finite-volume method
KW - Hydrofoil
KW - Large eddy simulation (LES)
KW - Sheet/cloud cavitation
KW - Shock waves
KW - Vortex shedding
KW - Weakly compressible flow
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U2 - 10.1016/j.apm.2005.11.019
DO - 10.1016/j.apm.2005.11.019
M3 - Article
AN - SCOPUS:33750842930
SN - 0307-904X
VL - 31
SP - 417
EP - 447
JO - Applied Mathematical Modelling
JF - Applied Mathematical Modelling
IS - 3
ER -