| Interaction 
 ANC-5 Strength of Metal Aircraft Elements	March 1955 Revised Edition     Section 1.535, pages 11-13
 
 
  
 |  | 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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