scholarly journals RADIOIODINE CONTROL DURING REPROCESSING OF SHORT-COOLED IRRADIATED $sup 237$Np ALUMINUM ALLOY TARGET ELEMENTS (A PRELIMINARY STUDY).

1967 ◽  
Author(s):  
W.O. Greenhalgh
Keyword(s):  
Aluminum Alloy ◽  
Alloy Target ◽  
Preliminary Study

scholarly journals Preliminary study on the microstructure and mechanical properties of dissimilar joints of aluminum alloy and pure copper by FSW

2017 ◽  
Vol 112 ◽  
pp. 04005 ◽  
Author(s):  
Daniela-Monica Iordache ◽  
Cătălin-Marian Ducu ◽  
Eduard-Laurentiu Niţu ◽  
Doina Iacomi ◽  
Adriana-Gabriela Plăiaşu
Keyword(s):  
Mechanical Properties ◽  
Aluminum Alloy ◽  
Pure Copper ◽  
Dissimilar Joints ◽  
Microstructure And Mechanical Properties ◽  
Preliminary Study

scholarly journals A preliminary study on the production of tritium from neutron-irradiated lithium-aluminum alloy.

RADIOISOTOPES ◽  
1982 ◽  
Vol 31 (11) ◽  
pp. 571-578 ◽  
Author(s):  
Masakazu TANASE ◽  
Koichi YAMAGUCHI ◽  
Kichizo TANAKA
Keyword(s):  
Aluminum Alloy ◽  
Lithium Aluminum ◽  
Preliminary Study

Preliminary Study on the Formability of a Laser-Welded Superplastic Aluminum Alloy

2014 ◽  
Vol 23 (11) ◽  
pp. 4154-4162 ◽  
Author(s):  
D. Sorgente ◽  
O. Corizzo ◽  
M. Brandizzi ◽  
L. Tricarico
Keyword(s):  
Aluminum Alloy ◽  
Preliminary Study

An Analysis of the Influence of Cutting Parameters on the Turning Process on the Fatigue Life of Aluminum Alloy UNS A92024-T351

2012 ◽  
Vol 498 ◽  
pp. 19-24 ◽  
Author(s):  
Alvaro Gómez ◽  
A. Sanz ◽  
Mariano Marcos Bárcena
Keyword(s):  
Aluminum Alloy ◽  
Fatigue Life ◽  
Fatigue Strength ◽  
Surface Condition ◽  
Cutting Parameters ◽  
Structural Elements ◽  
Turning Process ◽  
Machining Processes ◽  
Preliminary Study ◽  
The Relationship

Generally, metal structural elements of aircraft are placed in zones of critical load; in most cases, these elements are manufactured by machining processes. The fatigue life of these components is an important dynamic property that may be strongly affected by the surface condition produced during machining. In this paper a preliminary study of the influence of cutting parameters on fatigue strength of parts machined in aeronautical aluminum alloy UNS A92024-T351 has been carried out. Special attention has been provided to the relationship with surface finish evaluated through the roughness average.

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