Evaluation of various techniques for stress corrosion testing welded aluminum alloys.
Stress corrosion cracking resistance testing of high strength weldable aluminum alloys including residual stresses
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Stress corrosion cracking resistance testing of high strength weldable aluminum alloys including residual stresses
Because of such characteristics as high strength and long-term biocompatability, aerospace carbonaceous materials may be used as surgical implants to correct pathological conditions in the body resulting from disease or injury. Examples of possible medical uses include bone replacement, implantation splints and circulatory bypass implants.
Series of elements connected by idle rollers and two tapes /one for extension and one for retraction/ are used in the fabrication of a telescoping boom. The boom has high strength and rigidity which will allow a gravity dump at any point in the extension cycle.
Because introduction of hydrogen during bright-cadmium electroplating of high strength steels causes hydrogen-stress cracking, a program was undertaken to evaluate various processes and materials. Report describes effectiveness of inhibitors for reducing hydrogen absorption by steels.
Explosive bonding process produces sheet composites of aluminum alloy reinforced by high-strength stainless steel wires. The bonds are excellent metallurgically, no external heat is required, various metals can be bonded, and the process is inexpensive.
Stress corrosion cracking of high strength aluminum alloys investigated by electrochemical, mechanical, and electron microscopic techniques
Crack toughness characteristics of high strength alloys for use in heavy sections of supersonic aircraft
Hydrogen embrittlement and stress cracking studied on 14 selected high strength alloys
Mechanical property data on sheet and plate of high strength aluminum alloys
High temperature magnetic analysis of metallurgical structure of high strength steels and composites, including phase transformation and matrix grain structure
Wrought aluminum alloys provide high-strength substitute in the damaged area of aluminum castings. The segment can either be welded to the cast alloy or built in with a heat-treatable welding rod.
Gap welding of electronic interconnections yields high strength joints, is easy to use, and allows visual inspection of the welding process. It is easily adaptable to automated circuit assembly.
Iron-base and nickel-base alloys exhibit good oxidation resistance and improved ductility with addition of small amounts of yttrium, tantalum /or hafnium/, and thorium. They can be used in applications above the operating temperatures of the superalloys, if high strength materials are not required.
Cryogenic-liquid transfer system, containing a ring structure with tensioned small diameter, high strength wires, provides adequate physical support for the piping, minimizes the conductive heat paths between the piping and jacket, and allows for thermal expansion and contraction of the piping.
Mechanical properties, after thermal treatments, are summarized for sheet and plate of copper-rich, high-strength, heat-treatable aluminum-2021. The alloy is quench sensitive, quench rate and variations in aging affect corrosion behavior. Aging effects on yield strength, tensile strength, and elongation of sheet and plate are compared.
Metal lined boron and graphite composites exhibit high strength and minimum weight, making them superior to aluminum cylindrical shell structures and to steel or aluminum constructed pressure vessels. S glass filament-epoxy resin matrix with aluminum liner is suitable for cryogenic tanks.
High strength alloys, refractory metal, and ceramic materials for spacecraft structures
High strength reinforced metallic composites for applications over wide temperature range