Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 211
Fig. 117. Small Internal Mast and Its Attachment to Torque Tube 191 Control Systems Art. 137 … 192 Art. 138 General Comments be noted that a flange is put only on the compression side of the mast.One point of weakness in this mast, and often in other types, is throughsection B—B. A slight lateral component in the stress in the controlcable will cause the top of the mast to buckle sideways.…
Airplanes
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