Damping in Yaw and Static Directional Stability of a Canard Airplane Model and of Several Models Having Fuselages of Relatively Flat Cross Section
1950-10-16
Miscellaneous
No indication
English
Static stability of fuselages having relatively flat cross section
Engineering Index Backfile | 1955
|Shaping of airplane fuselages for minimum drag
AIAA | 1986
|