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Fabrication and evaluation of cold/formed/weldbrazed beta-titanium skin-stiffened compression panelsThe room temperature and elevated temperature buckling behavior of cold formed beta titanium hat shaped stiffeners joined by weld brazing to alpha-beta titanium skins was determined. A preliminary set of single stiffener compression panels were used to develop a data base for material and panel properties. These panels were tested at room temperature and 316 C (600 F). A final set of multistiffener compression panels were fabricated for room temperature tests by the process developed in making the single stiffener panels. The overall geometrical dimensions for the multistiffener panels were determined by the structural sizing computer code PASCO. The data presented from the panel tests include load shortening curves, local buckling strengths, and failure loads. Experimental buckling loads are compared with the buckling loads predicted by the PASCO code. Material property data obtained from tests of ASTM standard dogbone specimens are also presented.
Document ID
19830026829
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Royster, D. M.
(NASA Langley Research Center Hampton, VA, United States)
Bales, T. T.
(NASA Langley Research Center Hampton, VA, United States)
Davis, R. C.
(NASA Langley Research Center Hampton, VA, United States)
Wiant, H. R.
(Kentron International, Inc., Hampton Va., United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1983
Subject Category
Metallic Materials
Report/Patent Number
NASA-TP-2201
L-15634
NAS 1.60:2201
Report Number: NASA-TP-2201
Report Number: L-15634
Report Number: NAS 1.60:2201
Accession Number
83N35100
Funding Number(s)
PROJECT: RTOP 505-43-43-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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