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
1950-05-01
7 pages
Article (Journal)
Electronic Resource
English
Materials for aircraft structures
Engineering Index Backfile | 1950
|Composite materials for aircraft structures
SLUB | 1986
|Composite materials for aircraft structures
SLUB | 2004
|Composite Materials in Aircraft Structures
Emerald Group Publishing | 1989
Composite materials for aircraft structures
TIBKAT | 2016
|