Rules that must be followed in order to secure longitudinal stability and controllability and safety against stall in tail-first or Canard type airplane are determined for both conditions of power-off and power-on, whether high lift devices are operating or not; procedures for selection or determination of airfoil section, aspect ratio and area of tail surface, tail length and angle of setting of stabilizer are indicated.
Proportioning "Canard" airplane for longitudinal stability and safety against stall
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 9 , n 14
1942
6 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
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