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Static longitudinal stability and control of a convertible-type airplane as affected by articulated- and rigid-propeller operation
Report presenting the results of an investigation in the full-scale tunnel of the static longitudinal stability and control of a convertible-type airplane as affected by articulated- and rigid-propeller operation. The investigation included force measurements for a large angle-of-attack range with the all-movable horizontal tail installed and removed.
Date:
November 7, 1949
Creator:
Lange, Roy H. & McLemore, Huel C.
System:
The UNT Digital Library