Description of Boeing Supersonic Transport for which conventional skin-stringer panel construction has been selected for general use on wing, body, and empennage; general technical requirements are presented which led to selection of titanium alloys as basic structural material for Mach 2.7 transport; material properties such as strength, toughness, corrosion and stress corrosion resistance, metallurgical stability, and fatigue are considered, and fabrication characteristics are described. (see also Steel Oct 18 1965 p 128, 130)
Challenge of materials for supersonic transport
SAE -- Paper
SAE Meeting ; 1965 Titanium
Society of Automotive Engineers -- Papers ; 157 , n 16
1965
8 pages
Aufsatz (Konferenz)
Englisch
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The Challenge of Materials for the Supersonic Transport
SAE Technical Papers | 1965
|Structural materials for supersonic transport
Engineering Index Backfile | 1965
|Structural materials for supersonic transport
AIAA | 1965
|Structural materials for supersonic transport
AIAA | 1964
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