Accession Number:

AD0728698

Title:

Jet Deflection, Noise and Pressure Distribution in Proportional Amplifiers.

Descriptive Note:

Thesis,

Corporate Author:

NAVAL POSTGRADUATE SCHOOL MONTEREY CALIF

Personal Author(s):

Report Date:

1971-09-01

Pagination or Media Count:

131.0

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

Subject Categories:

  • Fluidics and Fluerics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE