Feasible region in general design space of lamination parameters for laminated composites

By C. Diaconu, Masaki Sato, H. Sekine. 2002

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Framework for the Buckling Optimization of Variable-Angle Tow Composite Plates (2015, methodology): “Figure A2 demonstrates the intersections of the feasible region with different planes, in which the solid lines represent the feasible region defined by the explicit formulas; the dashed lines indicate the true feasible region generated using a numerical procedure [12] and the outer boundary derived”
Optimum stacking sequence design of composite materials Part II: Variable stiffness design (2010, background): “require solving several optimization problems [19] and thus it is far more complicated than being incorporated into an optimization problem.”
Bilevel Optimization of Blended Composite Wing Panels (2011, methodology): “In addition, a group of relationships between the in-plane and out-ofplane lamination parameters for the symmetric laminates are available (see [12–15,30,31]).”