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High accuracy fuel flowmeterAll three flowmeter concepts (vortex, dual turbine, and angular momentum) were subjected to experimental and analytical investigation to determine the potential portotype performance. The three concepts were subjected to a comprehensive rating. Eight parameters of performance were evaluated on a zero-to-ten scale, weighted, and summed. The relative ratings of the vortex, dual turbine, and angular momentum flowmeters are 0.71, 1.00, and 0.95, respectively. The dual turbine flowmeter concept was selected as the primary candidate and the angular momentum flowmeter as the secondary candidate for prototype development and evaluation.
Document ID
19860021558
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Instrumentation And Photography
Report/Patent Number
NAS 1.26:174869
NASA-CR-174869
Report Number: NAS 1.26:174869
Report Number: NASA-CR-174869
Accession Number
86N31030
Funding Number(s)
CONTRACT_GRANT: NAS3-22139
PROJECT: RTOP 505-31-54
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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