HYDROJET DUCTED PROPULSION SYSTEM: IMPELLER INDUCED VIBRATORY PRESSURES AND PERFORMANCE CHARACTERISTICS
Abstract
A vortex-line theory developed for an impeller in a long duct was used to optimize the design of a Hydrojet impeller. A model Hydrojet with this impeller was instrumented for pressure field and impeller performance measurements. Fluctuating pressures were high near impeller but attenuate to <10% at 0.4D. 1st/2nd/3rd blade frequency harmonics were approximately in ratio of 1.0/0.6/0.25. 0.85 - 0.90 impeller efficiency appears possible.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1966
- Accession Number
- AD0664518
Entities
People
- Douglas H. Norrie
- Malcolm R. Hale
Organizations
- University of Adelaide