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Some cable suspension systems and their effects on the flexural frequencies of slender aerospace structuresThe effects of several cable suspension configurations on the first free-free flexural frequency of uniform beams have been determined by experiment and analysis. The results of this study confirm that in general the larger the test vehicle the larger is the flexural frequency measurement error attributable to a given cable suspension configuration. For horizontally oriented beams representing modern aerospace vehicles of average size and flexibility, the restraining effects of all but the shortest support cables were minor. The restraining effects of support cables of moderate length attached near the base of vertically oriented vehicles were overshadowed by the effects of beam compression due to gravity.
Document ID
19740025246
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Herr, R. W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-7693
L-9178
Report Number: NASA-TN-D-7693
Report Number: L-9178
Accession Number
74N33359
Funding Number(s)
PROJECT: RTOP 502-32-02-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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