A Potential Flow Solution on Marine Propeller and Axial Rotating Fan
Abstract
Integral equations are derived to model the solid surfaces and the inlet condition for both external and internal flows with an axially rotating element. Vortex filaments are used to simulate the lifting surfaces. Global iterations for surface-panel source densities and vortex strengths are used in conjunction with the Neumann iterations for solving integral equations. A special kernel treatment is adopted in the solution scheme of the integral equation. Solutions converge within 10-20 iterations. Calculated results and measured data for a propeller tested in open water are in good agreement. Predictions are also made for an axial-flow pump. The overall performance parameters for the pump agree within a few percent of the design values. Keywords: Propeller; Potential flow; Integral equation; Lifting surface; Vortex.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1988
- Accession Number
- ADA198781
Entities
People
- C. W. Jiang
- T. W. Bein
- Y. T. Lee