Tests of three airplanes conducted to develop elevators that would provide stick forces in steady turns within limits required by Army and Navy specifications; it is concluded that requirements for stick forces in steady turns and damping of control-free longitudinal oscillation are not adequate to assure satisfactory elevator control in all cases.
Investigation of additional requirements for satisfactory elevator control characteristics
Nat Advisory Committee Aeronautics -- Tech Note
1946
9 pages
Supp sheets, Bibliography
Aufsatz (Zeitschrift)
Englisch
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