The results of a study of folding tilt rotor (stowed rotor) aircraft are presented. The effects of design cruise speed on the gross weight of a conceptual design stowed rotor aircraft are shown and a comparison is made with a conventional (non-folding) tilt rotor aircraft. A flight research stowed rotor design is presented. The program plans, including costs and schedules, are shown for the research aircraft development and a wind tunnel plan is presented for a full scale test of the aircraft. (Author)
V/STOL Tilt Rotor Aircraft Study. Volume 5: Definition of Stowed Rotor Research Aircraft
1973
134 pages
Report
No indication
English
Stopped Stowed Rotor Composite Research Aircraft
NTIS | 1969
Rotor dynamics of a single stowed rotor aircraft
AIAA | 1969
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