Investigation in static test facility at Langley Laboratory is part of research program examining wing propeller configurations designed for VTOL and STOL applications; work extended to configuration having two propellers per semispan and covers effects of changes in vertical and longitudinal positions of propellers.
Effects of propeller position and overlap on slipstream deflection characteristics of wing-propeller configuration equipped with sliding and fowler flap
NACA -- Tech Note
NACA -- Technical Note ; n 4404
1958
81 pages
Report
Englisch
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