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User's manual for the Langley Research Center 14- by 22- foot subsonic tunnel static data acquisition systemThe Static Data Acquisition System (SDAS) components primarily responsible for acquiring data at the 14- by 22-Foot Subsonic Tunnel are the NEFF 620/600 Data Acquisition Unit (DAU) and the PSI 780B electronically scanned pressure (ESP) measurement system. A 9250 Modcomp computer is used to process the signal, to do all aerodynamic calculation, and to control the output of data. All of the tasks required to support a wind tunnel investigation are menu driven. The purpose of this report is to acquaint users of this system with the wide range of capabilities that exist with the available hardware and software and provide them with the proper procedures to follow when setting up or running individual tests.
Document ID
19940013166
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Orie, Nettie M.
(NASA Langley Research Center Hampton, VA, United States)
Quinto, P. Frank
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:109027
NASA-TM-109027
Report Number: NAS 1.15:109027
Report Number: NASA-TM-109027
Accession Number
94N17639
Funding Number(s)
PROJECT: RTOP 535-03-10-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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