General specifications of Rohr MO-1, two-place, side by side, incorporating all metal construction with cantilever wing surfaces and retractable tricycle landing gear; design is Canard type with stabilizing surfaces forward of wing and incorporates submerged engine installation under wing and just aft of passengers, which drives blower and pusher propeller at crankshaft speed; operating principles and advantages of canard design explained. (see also Aero Digest v 53 n 2 Aug 1946 p 90, 104, 1040)
Canard type light personal airplane
Automotive Aviation Industries
Automotive and Aviation Industries ; 95 , n 4
1946
Aufsatz (Zeitschrift)
Englisch
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Canard type light personal airplane
Engineering Index Backfile | 1946
|Investigation of some aerodynamic aspects of canard airplane
Engineering Index Backfile | 1945
|Free-spinning-tunnel tests of model of canard airplane
Engineering Index Backfile | 1943
|Proportioning "Canard" Airplane for longitudinal stability and safety against stall
Engineering Index Backfile | 1943
|Proportioning "Canard" airplane for longitudinal stability and safety against stall
Engineering Index Backfile | 1942
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