SUPERCAVITATING PROPELLER THEORY. PART I. THE DERIVATION OF INDUCED VELOCITY EQUATIONS AND FORMULATION OF AN INITIAL DESIGN PROCEDURE.
Abstract
Induced velocity equations are presented for supercavitating propellers along with a pressure equation. Blade loading is represented by a pressure doublet distribution and the blade cavity by a pressure source distribution. Subsequently, the pressure doublet distribution is transposed to the more familiar bound and free vorticity distribution. Lifting surface equations are presented for the case of induced advance ratio as a function of radius but attention is focused on the case of constant induced advance ratio. A simplified model is proposed where loading is considered to be concentrated along a line, i.e., the lifting line. For the case of constant induced advance ratio, an initial design procedure is formulated which incorporates the simplified model. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1966
- Accession Number
- AD0629735
Entities
People
- Geoffrey G. Cox