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An investigation of a thermal ice-prevention system for a C-46 cargo airplane 7: Effect of the thermal system on the wing-structure stresses as established in flight

Description: Report presenting an investigation of a thermal ice-prevention system for a Curtiss-Wright C-46 airplane, which included a determination of the change in stress at various locations in the wing outer panel caused by operation of the thermal system. Curves are presented showing the chordwise variation of stress and temperature for two wing stations.
Date: September 1945
Creator: Jones, Alun R.
Partner: UNT Libraries Government Documents Department