论文信息 - A BEM for the Prediction of Unsteady Midchord Face and/or Back Propeller Cavitation

A BEM for the Prediction of Unsteady Midchord Face and/or Back Propeller Cavitation

A boundary element method (BEM) is used for the numerical analysis of sheet cavitation on a propeller subjected to the non-axisymmetric wakes of marine vehicles. This method is extended in order to treat mixed partial and supercavity patterns on both the face and back of the blades with searched cavity detachment. The convergence of the method is studied

Y. L. Young | S. Kinnas

[1] L. Morino,et al. Subsonic Potential Aerodynamics for Complex Configurations: A General Theory , 1974 .

[2] Stuart D. Jessup,et al. Measurement of Multiple Blade Rate Unsteady Propeller Forces , 1990 .

[3] S. Kinnas. Leading-Edge Corrections to the Linear Theory of Partially Cavitating Hydrofoils , 1991 .

[4] S. Kinnas. A general theory for the coupling between thickness and loading for wings and propellers , 1992 .

[5] Spyridon A Kinnas,et al. Boundary element method for the analysis of the unsteady flow aroundextreme propeller geometries , 1992 .

[6] S. Kinnas,et al. A boundary element method for the analysis of the flow around 3-D cavitating hydrofoils , 1993 .

[7] S. Kinnas,et al. A numerical nonlinear analysis of the flow around two- and three-dimensional partially cavitating hydrofoils , 1993, Journal of Fluid Mechanics.

[8] Spyros A. Kinnas,et al. A NONLINEAR BOUNDARY ELEMENT METHOD FOR THE ANALYSIS OF UNSTEADY PROPELLER SHEET CAVITATION , 1994 .

[9] S. Kinnas,et al. Propeller sheet cavitation predictions using a panel method , 1999 .