This max to leads to the stress ratio redesign formula ta#39;/t = (N ) /N* , (G.3.4) where (N ) is the maximum shear stress resultant, and N* = x*t. sa#39;max s The value of ta#39;/t is chosen as the larger of (G.3.2) and (G.3.4); however, the user can suppressanbsp;...
|Title||:||DESAP 1: Theoretical and user's manual|
|Author||:||G. B. Reddy, United States. National Aeronautics and Space Administration|