NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Aeroacoustic flowmeterThe flowmeter is based on a measurement of phase difference between two points on the circumference of a pipe separated axially by an integral multiple of sound wavelength. Plane sound waves are generated aeroacoustically by a non-protruding ring cavity energized either directly by the flow or by a subsidiary flow of the same medium. The frequency of the aeroacoustic source varies with temperature and therefore the temperature can be obtained. In the case of steam flow, temperature can be measured independently and therefore from the measured frequency (or speed of sound), the quality of wet steam can be measured. The flowmeter is linear in velocity and no calibrations are required.
Document ID
20080008797
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Shakkottai, Parthasarathy
Kwack, Eug Y.
Date Acquired
August 24, 2013
Publication Date
January 30, 1990
Subject Category
Acoustics
Report/Patent Number
Patent Number: US-Patent-4,896,540
Patent Application Number: US-Patent-Appl-SN-179076
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-4,896,540
Patent Application
US-Patent-Appl-SN-179076
No Preview Available