Testing of the anemometer circuit : Data report
- Moen, Michael J.
- Mar 15, 1992.
- Physical Description:
- 1 electronic document
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- The 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.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19920024862.
Accession ID: 92N34106.
- No Copyright.
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