Interaction
ANC-5 Strength of Metal Aircraft Elements March 1955 Revised Edition Section 1.535, pages 11-13
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Section Factor
Elmer F. Bruhn Analysis and Design of Flight Vehicle Structures
Figure C3.8, page C3.3
t 1 / b = 0.125 / 1.375 = 0.091 t 2 / h = 0.125 / 2.00 = 0.0625 K = 1.166
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