Plane Stress Cyclic Flaw Growth of 2219- T87 Aluminum and 5 A1-2.5 SN ELI Titanium Alloys at Room and Cryogenic Temperatures Final Report, 1 Jul. 1964 - 1 May 1966
1966
153 pages
Report
Keine Angabe
Englisch
Iron & Iron Alloys , Crack propagation , Cryogenic temperature , Stress , Alloy , Aluminum , Crack , Cryogenic , Cyclic , Design , Fatigue , Flaw , Fracture , Fracture mechanics , Growth , Life , Liquid hydrogen , Mechanics , Propagation , Tank , Temperature , Titanium