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Test load verification through strain data analysisA traditional binding acceptance criterion on polycrystalline structures is the experimental verification of the ultimate factor of safety. At fracture, the induced strain is inelastic and about an order-of-magnitude greater than designed for maximum expected operational limit. At this extreme strained condition, the structure may rotate and displace at the applied verification load such as to unknowingly distort the load transfer into the static test article. Test may result in erroneously accepting a submarginal design or rejecting a reliable one. A technique was developed to identify, monitor, and assess the load transmission error through two back-to-back surface-measured strain data. The technique is programmed for expediency and convenience. Though the method was developed to support affordable aerostructures, the method is also applicable for most high-performance air and surface transportation structural systems.
Document ID
19950022297
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Verderaime, V.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Harrington, F.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
M-783
NASA-TP-3558
NAS 1.60:3558
Report Number: M-783
Report Number: NASA-TP-3558
Report Number: NAS 1.60:3558
Accession Number
95N28718
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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