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A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wingA technique which may be useful for selecting strain gages for use in load equations is described. The technique is an adaptation of the previously used T-value method and is applied to a multispar structure. The technique, called the modified T-value method, is used to reduce the number of strain gages used in a load equation from twelve to two. A parallel reduction is made by calculating relative equation accuracies from three applied load distributions. The equations developed from the modified T-value method proved to be accurate more consistently than the T-value method.
Document ID
19810003558
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Tang, M. H.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Sheldon, R. G.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1980
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TP-1748
H-1108
Accession Number
81N12066
Funding Number(s)
PROJECT: RTOP 505-33-54
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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