Tests of 4-ft diam ducted fan mounted on tip of semi-span wing for VTO L/STOL aircraft; effects of fan on aircraft longitudinal trim and control are examined over speed range corresponding to transition from hover to aircraft flight; evaluation of lateral control by differential thrust of fan.
Aerodynamics of tilting ducted fan configuration
NASA -- Tech Note
1961
15 pages
Aufsatz (Zeitschrift)
Englisch
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