Effects of Wing Sweep on Stability of a 5th-Generation Fighter Configuration
11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference
2011-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effects of Wing Sweep on Stability of a 5th-Generation Fighter Configuration
British Library Conference Proceedings | 2011
|Variable sweep wing configuration Patent
NTRS | 1962
|