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Wind tunnel real-time data acquisition systemThe hardware configuration is described for the data acquisition system (DAS) which consists of an analog front end that can process up to 260 channels of data, a multichannel analog-to-digital subsystem that can process up to 50,000 samples of data per second, and a digital computer with standard and nonstandard devices, including graphics capability. Also described are the software configuration of the DAS and complex hardware/software interfaces providing, for example, automatic amplifier gain and offset adjustment for each data channel. Specific DAS applications are summarized, including the real time processing of dynamic deflection data, unsteady pressure measurements, and flutter and buffet data.
Document ID
19790012926
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Cole, P.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1979
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TM-80081
Report Number: NASA-TM-80081
Accession Number
79N21097
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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