Example 9, Slide 6: Forward part of propellant tank showing inner orthogrid "layer", shell wall layer, external tapered doubler and support ring

Fig. 1c from the 2013 GENOPT paper1. Configuration of the forward part of the propellant tank in the neighborhood of the forward cylinder/dome junction. The names of several of the decision variable candidates are given. (See Tables 1, 2.)

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