Jet Deflection, Noise and Pressure Distribution in Proportional Amplifiers.
Abstract
The study presents the experimental work done on the determination of angle, noise, and pressure distribution for proportional amplifiers. The deflection angles were measured by means of a small, lightstring attached to a needle. The turbulence components in the three directions were obtained through the use of the hot-wire anemometer. The 'momentum balance' principal was employed to predict the deflection angles, by taking into account the effects of the momentum, static pressure, and centrifugal forces. The results so obtained were found to be in agreement with those obtained experimentally. The static wall pressures were obtained with a pressure transducer. The 'two dimensional-inviscid' flow model was used throughout the work. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1971
- Accession Number
- AD0728698
Entities
People
- Ercan Turken
Organizations
- Naval Postgraduate School