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Buckling tests of three 4.6 meter diameter aluminum honeycomb sandwich conical shells loaded under external pressureThree aluminum honeycomb sandwich conical shells with a 120 apex angle and a 4.6-m (15.0-ft) base diameter were loaded to failure by a uniform external pressure. The cones differed from one another only in the thickness of their respective face sheets. Test specimen details, test procedure, and test results are discussed. Both buckling and prebuckling data are compared with appropriate theoretical predictions, and good agreement was obtained between test and theory. Extensive imperfection measurements were made and reported on the three cones in the as fabricated condition.
Document ID
19750019348
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Anderson, J. K.
(NASA Langley Research Center Hampton, VA, United States)
Davis, R. C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
L-9936
NASA-TN-D-7935
Report Number: L-9936
Report Number: NASA-TN-D-7935
Accession Number
75N27420
Funding Number(s)
PROJECT: RTOP 505-02-42-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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