Damping in Yaw and Static Directional Stability of a Canard Airplane Model and of Several Models Having Fuselages of Relatively Flat Cross Section
16.10.1950
Sonstige
Keine Angabe
Englisch
Static stability of fuselages having relatively flat cross section
Engineering Index Backfile | 1955
|Shaping of airplane fuselages for minimum drag
AIAA | 1986
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