Fatigue behavior test program conducted on Ti-A1-Mo-V sheet metal in simulated wing structure under environment of supersonic transport
Fatigue behavior of Ti-8A1Mo-1V sheet in a simulated wing structure under the environment of a supersonic transport
1965-11-01
Report
Keine Angabe
Englisch
Oblique wing supersonic transport concepts
NTRS | 1992
|Oblique wing supersonic transport concepts
AIAA | 1992
|