Effect of skewed wing-tip controls on a variable-sweep wing-fuselage configuration
1967
93 S
graph. Darst
Buch
Englisch
Variable sweep wing configuration Patent
NTRS | 1962
|AIAA | 1983
|AIAA | 1980
Wing Pivot Assembly for Variable Sweep Wing Aircraft
NTIS | 1978
|WING-FUSELAGE FUSION TYPE VARIABLE OBLIQUE WING PLUS TERMINAL WING MISSILE
Europäisches Patentamt | 2017
|