Effects of fabrication and joining processes on compressive strength of boron/aluminum and borsic/aluminum structural panels
Technical Report
·
OSTI ID:6486567
Processes for forming and joining boron/aluminum and borsic/aluminum to themselves and to titanium alloys were studied. Composite skin and titanium skin panels were joined to composite stringers by high strength bolts, by spotwelding, by diffusion bonding, by adhesive bonding, or by brazing. The effects of the fabrication and joining processes on panel compressive strengths were discussed. Predicted buckling loads were compared with experimental data.
- Research Organization:
- National Aeronautics and Space Administration, Langley AFB, VA (USA). Langley Research Center
- OSTI ID:
- 6486567
- Report Number(s):
- N-78-20256; NASA-TP-1121; L-11728
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
36 MATERIALS SCIENCE
360101 -- Metals & Alloys-- Preparation & Fabrication
360301* -- Composite Materials-- Preparation & Fabrication-- (-1987)
360303 -- Composite Materials-- Mechanical Properties-- (-1987)
ALLOYS
ALUMINIUM
BONDING
BORON
BRAZING
COMPOSITE MATERIALS
COMPRESSION STRENGTH
ELEMENTS
FABRICATION
JOINING
MECHANICAL PROPERTIES
METALS
SEMIMETALS
TITANIUM ALLOYS
WELDING
360101 -- Metals & Alloys-- Preparation & Fabrication
360301* -- Composite Materials-- Preparation & Fabrication-- (-1987)
360303 -- Composite Materials-- Mechanical Properties-- (-1987)
ALLOYS
ALUMINIUM
BONDING
BORON
BRAZING
COMPOSITE MATERIALS
COMPRESSION STRENGTH
ELEMENTS
FABRICATION
JOINING
MECHANICAL PROPERTIES
METALS
SEMIMETALS
TITANIUM ALLOYS
WELDING