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Strain-gage bridge calibration and flight loads measurements on a low-aspect-ratio thin wingStrain-gage bridges were used to make in-flight measurements of bending moment, shear, and torque loads on a low-aspect-ratio, thin, swept wing having a full depth honeycomb sandwich type structure. Standard regression analysis techniques were employed in the calibration of the strain bridges. Comparison of the measured loads with theoretical loads are included.
Document ID
19750023957
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Peele, E. L.
(NASA Langley Research Center Hampton, VA, United States)
Eckstrom, C. V.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1975
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-7979
L-9896
Report Number: NASA-TN-D-7979
Report Number: L-9896
Accession Number
75N32030
Funding Number(s)
PROJECT: RTOP 505-02-22-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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