Review of 4-yr STOL Research Program conducted jointly by DeHavilland Aircraft of Canada and Canadian Defence Research Board; Otter aircraft which employs powerful double slotted flaps is fitted with enlarged flaps with novel aerodynamic features and used in studies to assess static stability and control problems; boundary layer control scheme adapted to requirement of flight aircraft; performance and stability tests, flight test and results.
Towards still shorter takeoffs and landings
Can Aeronautical J
Canadian Aeronautical Journal ; 6 , n 4
1960
4 pages
Article (Journal)
English
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