“Use Of 75ST In Structural Applications”

470140

01/01/1947

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
The material known as 75ST is a new high strength aluminum alloy that can be used in certain aircraft structural applications to effect a saving in weight or an increase in strength or both over designs using other alloys. However, the structural engineer should be well acquainted with the advantages and limitations of this material before utilizing it in design.
Meta TagsDetails
DOI
https://doi.org/10.4271/470140
Pages
15
Citation
SNYDER, G., and CROSSLAND, F., "“Use Of 75ST In Structural Applications”," SAE Technical Paper 470140, 1947, https://doi.org/10.4271/470140.
Additional Details
Publisher
Published
Jan 1, 1947
Product Code
470140
Content Type
Technical Paper
Language
English