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Dynamic Stability Instrumentation System (DSIS). Volume 1: Hardware descriptionThis paper is a hardware description manual for the Dynamic Stability Instrumentation System that is used in specific NASA Langley wind tunnels. The instrumentation system performs either a synchronous demodulation or a fast Fourier transform on dynamic balance strain gage signals, and ultimately computes aerodynamic coefficients. The DSIS consists of a double rack of instruments, a remote motor-generator set, two special stings each with motor driven shafts, and specially designed balances. The major components in the instrumentation rack include a personal computer, digital signal processor microcomputers, computer-controlled signal conditioners, function generator, digital multimeter, and an optional fast Fourier transform analyzer.
Document ID
19950012484
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jordan, T. L.
(NASA Langley Research Center Hampton, VA, United States)
Daniels, T. S.
(NASA Langley Research Center Hampton, VA, United States)
Hare, D. A.
(NASA Langley Research Center Hampton, VA, United States)
Boyden, R. P.
(NASA Langley Research Center Hampton, VA, United States)
Dress, D. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Subject Category
Computer Programming And Software
Report/Patent Number
NASA-TM-109160-VOL-1
NAS 1.15:109160-VOL-1
Report Number: NASA-TM-109160-VOL-1
Report Number: NAS 1.15:109160-VOL-1
Accession Number
95N18899
Funding Number(s)
PROJECT: RTOP 505-59-54-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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