THE EFFECT OF PROPELLER CAVITATION ON THRUST DEDUCTION, A THEORETICAL EXAMINATION,
Abstract
A simple, idealized, theoretical model is used to examine the effect of propeller cavitation on thrust deduction. This study has yielded not only a qualitative understanding of how the presence of cavitation results in a decrease in thrust deduction, but also a rough quantitative estimate of the conditions that result in zero thrust deduction. The findings verify statements made in a recently published Soviet Union report. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1964
- Accession Number
- AD0606967
Entities
People
- D. M. Nelson
Organizations
- Naval Air Weapons Station China Lake