English (United Kingdom)

https://curated-unify.zendy.io/wp-json/zendy-region/v1/featured_content/oa?rat=en

https://curated-unify.zendy.io/wp-json/zendy-region/v1/highlighted_journal/

Global: Zendy Plus annual

Presents the access of premium content as premium feature

Premium Content

Presents the keyphrase highlighting as premium feature

Keyphrase Highlighting

Presents the summarisation as premium feature

Summarisation

Insights

Presents the pdf analysis as premium feature

PDF Analysis

Presents the zaia usage as premium feature

ZAIA

Global: Zendy Tools annual

Global: Zendy Free Plan

Global: Zendy Tools monthly

Global: Zendy Plus monthly

The laser welding technology parameters of new V-1579 (Al-Mg-Sc) and V-1481 (Al-Cu-Li) alloys were investigated. Weldability of such alloys was studied. Laser welding conditions and filler materials were selected to provide high weld ductility and impact strength. It was found that weld strength in regard to the parent material was ca. 0.8 for V-1481 alloy and ca. 0.9 for V-1579 alloy. Structurally similar samples of welded fuselage panel were manufactured based on conducted research. Weld inspection was carried out.

Laser welding of fuselage panels from aluminum V-1579 and aluminum-lithium V-1481 alloys