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Advanced beaded and tubular structural panelsA program to develop lightweight beaded and tubular structural panels is described. Applications include external surfaces, where aerodynamically acceptable, and primary structure protected by heat shields. The design configurations were optimized and selected with a computer code which iterates geometric parameters to satisfy strength, stability, and weight constraints. Methods of fabricating these configurations are discussed. Nondestructive testing produced extensive combined compression, shear, and bending test data on local buckling specimens and large panels. The optimized design concepts offer 25 to 30% weight savings compared to conventional stiffened sheet construction.
Document ID
19750022530
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Musgrove, M. D.
(Boeing Co. Seattle, WA, United States)
Greene, B. E.
(Boeing Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-2514
Report Number: NASA-CR-2514
Accession Number
75N30603
Funding Number(s)
CONTRACT_GRANT: NAS1-10749
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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