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Testing of the anemometer circuit: Data reportThe following text discusses results from the electronic step testing and the beginning of velocity step testing in the shock tube. It should be kept in mind that frequency response is always measured as the time from the beginning of the event to the minimum (positive inflection) of the 'bucket' that immediately follows the response. This report is not a complete account of the results from square wave testing. Some data is still in the process of being analyzed and efforts are being made to fit the data to both Freymuth's third order theory and modelled responses from SPICE circuit simulation software.
Document ID
19920024862
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Moen, Michael J.
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
September 6, 2013
Publication Date
March 15, 1992
Subject Category
Instrumentation And Photography
Report/Patent Number
NAS 1.26:190623
NASA-CR-190623
Report Number: NAS 1.26:190623
Report Number: NASA-CR-190623
Accession Number
92N34106
Funding Number(s)
CONTRACT_GRANT: NAG1-1201
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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