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Test of superplastically formed corrugated aluminum compression specimens with beaded websCorrugated wall sections provide a highly efficient structure for carrying compressive loads in aircraft and spacecraft fuselages. The superplastic forming (SPF) process offers a means to produce complex shells and panels with corrugated wall shapes. A study was made to investigate the feasibility of superplastically forming 7475-T6 aluminum sheet into a corrugated wall configuration and to demonstrate the structural integrity of the construction by testing. The corrugated configuration selected has beaded web segments separating curved-cap segments. Eight test specimens were fabricated. Two specimens were simply a single sheet of aluminum superplastically formed to a beaded-web, curved-cap corrugation configuration. Six specimens were single-sheet corrugations modified by adhesive bonding additional sheet material to selectively reinforce the curved-cap portion of the corrugation. The specimens were tested to failure by crippling in end compression at room temperature.
Document ID
19910019059
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Davis, Randall C.
(NASA Langley Research Center Hampton, VA., United States)
Royster, Dick M.
(NASA Langley Research Center Hampton, VA., United States)
Bales, Thomas T.
(NASA Langley Research Center Hampton, VA., United States)
James, William F.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Shinn, Joseph M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1991
Subject Category
Metallic Materials
Report/Patent Number
NAS 1.15:104119
NASA-TM-104119
Accession Number
91N28373
Funding Number(s)
PROJECT: RTOP 510-02-13-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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