Fatigue Behavior of a Fusion Welded Ti 8 A1 1 M0 1 V Simulated Wing Structure under the Environment of a Supersonic Transport
1967
76 pages
Report
Keine Angabe
Englisch
Aircraft , Fatigue test , Fused metal , Fusion welding , Structural fatigue , Supersonic transport , Amplitude , Annealing , Beam , Behavior , Box , Fatigue , Fuse , Fusion , Metal , Molybdenum , Skin , Spectrum , Stringer , Structural , Supersonic , Test , Titanium , Transport , Welding
Oblique wing supersonic transport concepts
NTRS | 1992
|Oblique wing supersonic transport concepts
AIAA | 1992
|