Two-place aircraft powered by Lycoming T-53 free turbine engine; gross weight 3200 lb; wing span 24 ft 11 in.; length 26 ft 5 in.; test shows feasibility of tilt wing principle; ease with which conversions can be accomplished and versatility of this type in both VTOL and STOL flights, demonstrated.
Design aspects and flight testing vertol 76 tilt-wing VTOL/STOL research aircraft
ASME -- Paper
ASME Meeting A-278 ; 1958 Vertical takeoff
1958
4 pages
Conference paper
English
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Engineering Index Backfile | 1957
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|Flight study of conversion maneuver of tilt-wing VTOL aircraft
Engineering Index Backfile | 1959
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