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Statistical load data processingA recorder system has been installed on two operational fighter aircrafts. Signal values from a c.g.-acceleration transducer and a strain-gage installation at the wing root were sampled and recorded in digital format on the recorder system. To analyse such load-time histories for fatigue evaluation purposes, a number of counting methods are available in which level crossings, peaks, or ranges are counted. Ten different existing counting principles are defined. The load-time histories are analysed to evaluate these counting methods. For some of the described counting methods, the counting results might be affected by arbitrarily chosen parameters such as the magnitude of load ranges that will be neglected and other secondary counting restrictions. Such influences might invalidate the final counting results entirely. The evaluation shows that for the type of load-time histories associated with most counting methods, a sensible value of the parameters involved can be found.
Document ID
19720022262
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vandijk, G. M.
(National Aerospace Lab. Amsterdam, Netherlands)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Publication Information
Publication: NASA. Langley Res. Center Advanced Approaches to Fatigue Evaluation
Subject Category
Structural Mechanics
Accession Number
72N29912
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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