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Visual display and alarm system for wind tunnel static and dynamic loadsA wind tunnel balance monitor and alarm system developed at NASA Ames Research Center will produce several beneficial results. The costs of wind tunnel delays because of inadvertent balance damage and the costs of balance repair or replacement can be greatly reduced or eliminated with better real-time information on the balance static and dynamic loading. The wind tunnel itself will have enhanced utility with the elimination of overly cautious limits on test conditions. The microprocessor-based system features automatic scaling and 16 multicolored LED bargraphs to indicate both static and dynamic components of the signals from eight individual channels. Five individually programmable alarm levels are available with relay closures for internal or external visual and audible warning devices and other functions such as automatic activation of external recording devices, model positioning mechanisms, or tunnel shutdown.
Document ID
19870010865
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hanly, Richard D.
(NASA Ames Research Center Moffett Field, CA, United States)
Fogarty, James T.
(Raman Aeronautics Research and Engineering, Inc. Palo Alto, Calif., United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.15:89455
A-87105
NASA-TM-89455
Report Number: NAS 1.15:89455
Report Number: A-87105
Report Number: NASA-TM-89455
Accession Number
87N20298
Funding Number(s)
PROJECT: RTOP 505-61-91
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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