In this article the author discusses the suitability of existing materials for aircraft structures and shows that a hypothetical material derived by expanding an aluminium alloy would greatly simplify the structure of fuselages
Materials for Aircraft Structures
Aircraft Engineering and Aerospace Technology ; 22 , 5 ; 146-152
01.05.1950
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Materials for aircraft structures
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