Results of some of developments, carried out recently by de Havilland Aircraft of Canada Ltd, are presented with respect to basic STOL performance, and low-speed control and handling; classical STOL deflected slipstream configuration and some of its limitations are reviewed; some improvements to basic design approach and in longitudinal low-speed control are discussed; other criteria are reviewed; flight-test results obtained with experimental aircraft incorporating modified longitudinal control system are discussed.
Some recent aerodynamic advances in STOL aircraft
J Aircraft
Journal of Aircraft ; 2 , n 5
1965
8 pages
Aufsatz (Zeitschrift)
Englisch
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